IRIDE-MS2-HEO-4, 64582
Orbit data source: Space-Track
IRIDE-MS2-HEO-4, 64582 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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64582 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: 12 hours ago
TLE from 12 hours ago
0 IRIDE-MS2-HEO-4
1 64582U 25135BG 26171.46968689 .00001498 00000-0 15336-3 0 9997
2 64582 97.7730 285.7706 0001775 33.5839 326.5492 14.91983067 54385Epoch: 2026-06-20T11:16Z
TLE epoch observation values (Epoch: 2026-06-20T11:16:20.947Z)
Latitude
-0.00002°
Longitude
-152.00053°
Altitude
593.762 km
Speed
7.564 km/s
True Right ascension
19h 03m 04s
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
10:19:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.009 km
Perigee altitude
587.535 km
Semi-major axis
6,966.909 km
Eccentricity
0.00018
Inclination
97.773°
RAAN
285.7706°
Arg. of periapsis
33.5839°
True anomaly
326.53799°
Mean anomaly
326.5492°
Eccentric anomaly
326.54359°
Mean motion
3.73236 °/min
Orbital period
96.45 mins
BSTAR
0.00015336
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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-4 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 06:44:48.307Z | 105.55° ESE | 2026-06-21 06:46:48.307Z | 70.054° E | 19.639° | 2026-06-21 06:49:48.307Z | 21.107° NNE |
| 6 mins | 2026-06-21 08:19:48.307Z | 211.764° SW | 2026-06-21 08:21:48.307Z | 250.143° W | 26.111° | 2026-06-21 08:25:48.307Z | 324.654° NNW |
| 6 mins | 2026-06-21 20:02:48.307Z | 36.102° NE | 2026-06-21 20:05:48.307Z | 107.861° ESE | 32.208° | 2026-06-21 20:08:48.307Z | 164.559° S |
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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