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: 8 hours ago
TLE from 8 hours ago
0 IRIDE-MS2-HEO-4
1 64582U 25135BG 26062.49885034 .00003119 00000-0 29833-3 0 9990
2 64582 97.7592 178.1926 0003847 349.6321 10.4819 14.93936150 38128Epoch: 2026-03-03T11:58Z
TLE epoch observation values (Epoch: 2026-03-03T11:58:20.669Z)
Latitude
-0.00001°
Longitude
-162.67056°
Altitude
586.087 km
Speed
7.569 km/s
True Right ascension
11h 52m 46s
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
23:38:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.371 km
Perigee altitude
580.015 km
Semi-major axis
6,960.83 km
Eccentricity
0.00038
Inclination
97.7592°
RAAN
178.1926°
Arg. of periapsis
349.6321°
True anomaly
10.48992°
Mean anomaly
10.4819°
Eccentric anomaly
10.48591°
Mean motion
3.73725 °/min
Orbital period
96.33 mins
BSTAR
0.00029833
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 20:34:40.535Z | 9.834° NNE | 2026-03-03 20:37:40.535Z | 336.971° NNW | 44.195° | 2026-03-03 20:41:40.535Z | 196.872° SSW |
| 6 mins | 2026-03-04 07:24:40.535Z | 143.734° SSE | 2026-03-04 07:26:40.535Z | 76.456° E | 40.51° | 2026-03-04 07:30:40.535Z | 355.878° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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