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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 IRIDE-MS2-HEO-8
1 64587U 25135BM 26035.60810002 .00022468 00000-0 11861-2 0 9990
2 64587 97.2676 154.2015 0202873 192.2027 167.4245 14.99459477 34119Epoch: 2026-02-04T14:35Z
TLE epoch observation values (Epoch: 2026-02-04T14:35:39.841Z)
Latitude
-0.00002°
Longitude
160.51326°
Altitude
709.343 km
Speed
7.426 km/s
True Right ascension
10h 16m 48s
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
07:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
706.42 km
Perigee altitude
424.682 km
Semi-major axis
6,943.688 km
Eccentricity
0.02029
Inclination
97.2676°
RAAN
154.2015°
Arg. of periapsis
192.2027°
True anomaly
167.91842°
Mean anomaly
167.4245°
Eccentric anomaly
167.67266°
Mean motion
3.75109 °/min
Orbital period
95.97 mins
BSTAR
0.0011861
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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 | 2026-02-05 06:45:34.752Z | 111.928° ESE | 2026-02-05 06:48:34.752Z | 71.261° E | 18.723° | 2026-02-05 06:51:34.752Z | 26.559° NE |
| 7 mins | 2026-02-05 08:20:34.752Z | 199.012° SSW | 2026-02-05 08:23:34.752Z | 261.596° W | 34.284° | 2026-02-05 08:27:34.752Z | 331.938° NNW |
| 4 mins | 2026-02-05 20:01:34.752Z | 50.552° ENE | 2026-02-05 20:03:34.752Z | 98.462° ESE | 22.983° | 2026-02-05 20:05:34.752Z | 144.106° SSE |
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
Authenticating...
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