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: 11 hours ago
TLE from 11 hours ago
0 IRIDE-MS2-HEO-8
1 64587U 25135BM 25328.19286759 .00003471 00000-0 33580-3 0 9990
2 64587 97.7593 80.2291 0003352 309.1448 50.9474 14.93416052 23308Epoch: 2025-11-24T04:37Z
TLE epoch observation values (Epoch: 2025-11-24T04:37:43.759Z)
Latitude
0.00001°
Longitude
-52.59959°
Altitude
588.867 km
Speed
7.566 km/s
True Right ascension
05h 20m 54s
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
12:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.644 km
Perigee altitude
581.976 km
Semi-major axis
6,962.447 km
Eccentricity
0.00034
Inclination
97.7593°
RAAN
80.2291°
Arg. of periapsis
309.1448°
True anomaly
50.97724°
Mean anomaly
50.9474°
Eccentric anomaly
50.96232°
Mean motion
3.73594 °/min
Orbital period
96.36 mins
BSTAR
0.0003358
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-24 19:41:25.356Z | 50.386° ENE | 2025-11-24 19:43:25.356Z | 84.754° E | 21.095° | 2025-11-24 19:46:25.356Z | 140.79° SSE |
| 5 mins | 2025-11-24 21:17:25.356Z | 330.254° NNW | 2025-11-24 21:19:25.356Z | 286.973° WNW | 24.152° | 2025-11-24 21:22:25.356Z | 235.804° WSW |
| 5 mins | 2025-11-25 08:06:25.356Z | 204.383° SW | 2025-11-25 08:08:25.356Z | 259.823° W | 33.903° | 2025-11-25 08:11:25.356Z | 327.468° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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