IRIDE-MS1-EAG2-9, 68449
Orbit data source: Space-Track
IRIDE-MS1-EAG2-9, 68449 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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68449 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IRIDE-MS1-EAG2-9
1 68449U 26067AK 26259.16561829 .00007146 00000-0 34406-3 0 9992
2 68449 97.4611 216.2728 0005933 103.2665 256.9232 15.19049361 25748Epoch: 2026-09-16T03:58Z
TLE epoch observation values (Epoch: 2026-09-16T03:58:29.420Z)
Latitude
0.00004°
Longitude
161.52909°
Altitude
512.727 km
Speed
7.607 km/s
True Right ascension
14h 25m 05s
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
04:04:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.766 km
Perigee altitude
501.598 km
Semi-major axis
6,883.819 km
Eccentricity
0.00059
Inclination
97.4611°
RAAN
216.2728°
Arg. of periapsis
103.2665°
True anomaly
256.85699°
Mean anomaly
256.9232°
Eccentric anomaly
256.89009°
Mean motion
3.80013 °/min
Orbital period
94.73 mins
BSTAR
0.00034406
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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-EAG2-9 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-17 21:11:48.805Z | 162.505° S | 2026-09-17 21:15:48.805Z | 13.99° NNE | 65.278° | 2026-09-17 21:18:48.805Z | 351.081° N |
| 6 mins | 2026-09-18 10:17:48.805Z | 2.202° NNE | 2026-09-18 10:19:48.805Z | 323.745° NNW | 59.46° | 2026-09-18 10:23:48.805Z | 202.43° 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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