IRIDE-MS2-HEO-8, 64587
Orbit data source: Space-Track
IRIDE-MS2-HEO-8, 64587 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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64587 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-8
1 64587U 25135BM 26133.26255757 .00001214 00000-0 12571-3 0 9997
2 64587 97.7692 248.2408 0003078 100.6478 259.5088 14.91864459 48699Epoch: 2026-05-13T06:18Z
TLE epoch observation values (Epoch: 2026-05-13T06:18:04.974Z)
Latitude
0.00005°
Longitude
-77.30503°
Altitude
595.555 km
Speed
7.562 km/s
True Right ascension
16h 32m 57s
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
22:52:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.286 km
Perigee altitude
586.997 km
Semi-major axis
6,967.278 km
Eccentricity
0.00031
Inclination
97.7692°
RAAN
248.2408°
Arg. of periapsis
100.6478°
True anomaly
259.47412°
Mean anomaly
259.5088°
Eccentric anomaly
259.49146°
Mean motion
3.73206 °/min
Orbital period
96.46 mins
BSTAR
0.00012571
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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-8 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 | 2026-05-13 19:45:22.186Z | 41.485° NE | 2026-05-13 19:48:22.186Z | 91.134° ESE | 22.879° | 2026-05-13 19:51:22.186Z | 146.162° SSE |
| 5 mins | 2026-05-13 21:22:22.186Z | 325.566° NNW | 2026-05-13 21:24:22.186Z | 282.542° WNW | 22.507° | 2026-05-13 21:27:22.186Z | 236.265° WSW |
| 6 mins | 2026-05-14 08:11:22.186Z | 202.63° SW | 2026-05-14 08:14:22.186Z | 278.211° WNW | 30.906° | 2026-05-14 08:17:22.186Z | 328.53° NNW |
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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