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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS2-HEO-9
1 64585U 25135BK 26046.27338105 .00003848 00000-0 36709-3 0 9992
2 64585 97.7617 162.2895 0004938 49.5968 310.5682 14.93907793 35707Epoch: 2026-02-15T06:33Z
TLE epoch observation values (Epoch: 2026-02-15T06:33:40.122Z)
Latitude
-0.00005°
Longitude
-81.41212°
Altitude
586.574 km
Speed
7.568 km/s
True Right ascension
10h 49m 09s
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
16:36:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.218 km
Perigee altitude
579.344 km
Semi-major axis
6,960.918 km
Eccentricity
0.00049
Inclination
97.7617°
RAAN
162.2895°
Arg. of periapsis
49.5968°
True anomaly
310.5252°
Mean anomaly
310.5682°
Eccentric anomaly
310.5467°
Mean motion
3.73717 °/min
Orbital period
96.33 mins
BSTAR
0.00036709
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-15 19:59:57.848Z | 35.631° NE | 2026-02-15 20:02:57.848Z | 99.31° ESE | 30.945° | 2026-02-15 20:05:57.848Z | 160.951° S |
| 5 mins | 2026-02-16 06:49:57.848Z | 107.793° ESE | 2026-02-16 06:51:57.848Z | 68.767° E | 21.656° | 2026-02-16 06:54:57.848Z | 18.222° NNE |
| 5 mins | 2026-02-16 08:24:57.848Z | 218.028° SW | 2026-02-16 08:26:57.848Z | 256.278° W | 23.486° | 2026-02-16 08:29:57.848Z | 314.606° 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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