IRIDE-MS2-HEO-9, 64585
Orbit data source: Space-Track
IRIDE-MS2-HEO-9, 64585 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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64585 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: 5 hours ago
TLE from 5 hours ago
0 IRIDE-MS2-HEO-9
1 64585U 25135BK 26120.20827763 .00000839 00000-0 86048-4 0 9990
2 64585 97.7697 235.3922 0003919 134.7794 225.3745 14.93055649 46743Epoch: 2026-04-30T04:59Z
TLE epoch observation values (Epoch: 2026-04-30T04:59:55.187Z)
Latitude
0.00002°
Longitude
-57.74593°
Altitude
593.376 km
Speed
7.562 km/s
True Right ascension
15h 41m 34s
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
17:27:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.161 km
Perigee altitude
582.703 km
Semi-major axis
6,963.569 km
Eccentricity
0.00039
Inclination
97.7697°
RAAN
235.3922°
Arg. of periapsis
134.7794°
True anomaly
225.34255°
Mean anomaly
225.3745°
Eccentric anomaly
225.35852°
Mean motion
3.73504 °/min
Orbital period
96.38 mins
BSTAR
0.000086048
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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-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 | 2026-04-30 20:02:50.673Z | 31.733° NE | 2026-04-30 20:05:50.673Z | 86.829° E | 31.931° | 2026-04-30 20:09:50.673Z | 167.409° S |
| 4 mins | 2026-04-30 21:39:50.673Z | 318.446° NNW | 2026-04-30 21:40:50.673Z | 302.061° NW | 15.526° | 2026-04-30 21:43:50.673Z | 255.262° W |
| 5 mins | 2026-05-01 06:53:50.673Z | 104.762° ESE | 2026-05-01 06:55:50.673Z | 61.36° ENE | 22.831° | 2026-05-01 06:58:50.673Z | 14.426° NNE |
| 5 mins | 2026-05-01 08:28:50.673Z | 223.355° SW | 2026-05-01 08:30:50.673Z | 262.741° W | 22.53° | 2026-05-01 08:33:50.673Z | 315.753° 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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