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: 9 hours ago
TLE from 9 hours ago
0 IRIDE-MS2-HEO-9
1 64585U 25135BK 26171.58161628 .00001273 00000-0 13124-3 0 9995
2 64585 97.7767 286.0674 0001900 42.6505 317.4861 14.91976475 54404Epoch: 2026-06-20T13:57Z
TLE epoch observation values (Epoch: 2026-06-20T13:57:31.646Z)
Latitude
-0.00004°
Longitude
167.89137°
Altitude
593.839 km
Speed
7.564 km/s
True Right ascension
19h 04m 16s
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
10:19:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.116 km
Perigee altitude
587.469 km
Semi-major axis
6,966.93 km
Eccentricity
0.00019
Inclination
97.7767°
RAAN
286.0674°
Arg. of periapsis
42.6505°
True anomaly
317.47138°
Mean anomaly
317.4861°
Eccentric anomaly
317.47874°
Mean motion
3.73234 °/min
Orbital period
96.45 mins
BSTAR
0.00013124
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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 | 2026-06-21 07:47:21.654Z | 173.961° S | 2026-06-21 07:50:21.654Z | 227.666° WSW | 43.556° | 2026-06-21 07:54:21.654Z | 343.434° N |
| 4 mins | 2026-06-21 19:32:21.654Z | 68.959° E | 2026-06-21 19:33:21.654Z | 85.898° E | 16.352° | 2026-06-21 19:36:21.654Z | 133.476° SE |
| 5 mins | 2026-06-21 21:07:21.654Z | 339.325° N | 2026-06-21 21:09:21.654Z | 290.339° WNW | 30.297° | 2026-06-21 21:12:21.654Z | 228.021° WSW |
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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