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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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: 6 hours ago
TLE from 6 hours ago
0 IRIDE-MS2-HEO-4
1 64582U 25135BG 25328.54849110 .00002851 00000-0 27950-3 0 9995
2 64582 97.7589 80.5149 0002868 301.0332 59.0605 14.93028760 23353Epoch: 2025-11-24T13:09Z
TLE epoch observation values (Epoch: 2025-11-24T13:09:49.631Z)
Latitude
-0.00006°
Longitude
179.31123°
Altitude
590.514 km
Speed
7.565 km/s
True Right ascension
05h 22m 03s
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
16:05:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.512 km
Perigee altitude
583.518 km
Semi-major axis
6,963.652 km
Eccentricity
0.00029
Inclination
97.7589°
RAAN
80.5149°
Arg. of periapsis
301.0332°
True anomaly
59.08869°
Mean anomaly
59.0605°
Eccentric anomaly
59.0746°
Mean motion
3.73497 °/min
Orbital period
96.39 mins
BSTAR
0.0002795
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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 | 2025-11-24 20:09:45.022Z | 24.192° NE | 2025-11-24 20:13:45.022Z | 114.885° SE | 37.451° | 2025-11-24 20:16:45.022Z | 173.258° S |
| 5 mins | 2025-11-25 07:00:45.022Z | 117.045° SE | 2025-11-25 07:02:45.022Z | 70.747° E | 27.516° | 2025-11-25 07:05:45.022Z | 13.3° NNE |
| 4 mins | 2025-11-25 08:36:45.022Z | 237.832° WSW | 2025-11-25 08:38:45.022Z | 275.472° WNW | 18.173° | 2025-11-25 08:40:45.022Z | 307.27° NW |
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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