IRIDE-MS2-HEO-4, 64582
Orbit data source: Space-Track
IRIDE-MS2-HEO-4, 64582 is an Italian payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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64582 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
ArgoTec
Mission
Operational Civil Imaging
Bus & Motor
HAWK, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
0.683 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 IRIDE-MS2-HEO-4
1 64582U 25135BG 26260.26661300 .00001626 00000-0 16617-3 0 9990
2 64582 97.7802 13.3855 0002159 69.7914 290.3537 14.91957665 67621Epoch: 2026-09-17T06:23Z
TLE epoch observation values (Epoch: 2026-09-17T06:23:55.363Z)
Latitude
0.00001°
Longitude
-78.80149°
Altitude
594.35 km
Speed
7.563 km/s
True Right ascension
00h 53m 32s
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
07:19:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.356 km
Perigee altitude
587.347 km
Semi-major axis
6,966.988 km
Eccentricity
0.00022
Inclination
97.7802°
RAAN
13.3855°
Arg. of periapsis
69.7914°
True anomaly
290.3305°
Mean anomaly
290.3537°
Eccentric anomaly
290.3421°
Mean motion
3.73229 °/min
Orbital period
96.46 mins
BSTAR
0.00016617
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-MS2-HEO-4 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 19:51:28.641Z | 41.809° NE | 2026-09-17 19:54:28.641Z | 100.414° ESE | 29.229° | 2026-09-17 19:57:28.641Z | 153.908° SSE |
| 4 mins | 2026-09-17 21:28:28.641Z | 316.783° NNW | 2026-09-17 21:29:28.641Z | 296.996° NW | 21.68° | 2026-09-17 21:32:28.641Z | 245.845° WSW |
| 4 mins | 2026-09-18 06:42:28.641Z | 99.339° ESE | 2026-09-18 06:44:28.641Z | 63.273° ENE | 19.574° | 2026-09-18 06:46:28.641Z | 29.845° NE |
| 5 mins | 2026-09-18 08:17:28.641Z | 213.43° SW | 2026-09-18 08:19:28.641Z | 259.207° W | 32.744° | 2026-09-18 08:22:28.641Z | 320.824° NNW |
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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