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 26062.54885360 .00003467 00000-0 33020-3 0 9990
2 64585 97.7629 178.3726 0003514 2.9454 357.1786 14.94039911 38134Epoch: 2026-03-03T13:10Z
TLE epoch observation values (Epoch: 2026-03-03T13:10:20.951Z)
Latitude
-0°
Longitude
179.45898°
Altitude
585.955 km
Speed
7.569 km/s
True Right ascension
11h 53m 29s
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
21:48:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.816 km
Perigee altitude
579.924 km
Semi-major axis
6,960.507 km
Eccentricity
0.00035
Inclination
97.7629°
RAAN
178.3726°
Arg. of periapsis
2.9454°
True anomaly
357.17662°
Mean anomaly
357.1786°
Eccentric anomaly
357.17761°
Mean motion
3.73751 °/min
Orbital period
96.32 mins
BSTAR
0.0003302
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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 | 2026-03-03 20:09:54.508Z | 24.399° NE | 2026-03-03 20:13:54.508Z | 110.701° ESE | 37.05° | 2026-03-03 20:16:54.508Z | 172.044° S |
| 5 mins | 2026-03-04 07:00:54.508Z | 110.521° ESE | 2026-03-04 07:02:54.508Z | 60.563° ENE | 26.366° | 2026-03-04 07:05:54.508Z | 11.081° NNE |
| 4 mins | 2026-03-04 08:36:54.508Z | 244.277° WSW | 2026-03-04 08:37:54.508Z | 263.829° W | 18.878° | 2026-03-04 08:40:54.508Z | 312.504° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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