IRIDE-MS1-EAG2-16, 68452
Orbit data source: Space-Track
IRIDE-MS1-EAG2-16, 68452 is an Italian payload satellite in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68452 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IRIDE-MS1-EAG2-16
1 68452U 26067AN 26259.15948806 .00007017 00000-0 33743-3 0 9999
2 68452 97.4646 216.3623 0006063 98.1959 261.9963 15.19097371 25749Epoch: 2026-09-16T03:49Z
TLE epoch observation values (Epoch: 2026-09-16T03:49:39.768Z)
Latitude
-0.00005°
Longitude
163.83153°
Altitude
512.239 km
Speed
7.607 km/s
True Right ascension
14h 25m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:05:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.71 km
Perigee altitude
501.363 km
Semi-major axis
6,883.674 km
Eccentricity
0.00061
Inclination
97.4646°
RAAN
216.3623°
Arg. of periapsis
98.1959°
True anomaly
261.92751°
Mean anomaly
261.9963°
Eccentric anomaly
261.9619°
Mean motion
3.80026 °/min
Orbital period
94.73 mins
BSTAR
0.00033743
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDE-MS1-EAG2-16 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 21:03:23.557Z | 152.82° SSE | 2026-09-17 21:06:23.557Z | 89.638° E | 57.175° | 2026-09-17 21:09:23.557Z | 359.124° N |
| 5 mins | 2026-09-18 10:09:23.557Z | 11.123° NNE | 2026-09-18 10:11:23.557Z | 294.013° NW | 87.698° | 2026-09-18 10:14:23.557Z | 193.97° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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