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 26224.58698008 .00000820 00000-0 86425-4 0 9990
2 64582 97.7771 338.1720 0002687 124.5884 235.5589 14.91984370 62308Epoch: 2026-08-12T14:05Z
TLE epoch observation values (Epoch: 2026-08-12T14:05:15.078Z)
Latitude
-0.00001°
Longitude
165.8204°
Altitude
595.85 km
Speed
7.561 km/s
True Right ascension
22h 32m 41s
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
16:55:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.64 km
Perigee altitude
586.896 km
Semi-major axis
6,966.905 km
Eccentricity
0.00027
Inclination
97.7771°
RAAN
338.172°
Arg. of periapsis
124.5884°
True anomaly
235.53351°
Mean anomaly
235.5589°
Eccentric anomaly
235.54621°
Mean motion
3.73236 °/min
Orbital period
96.45 mins
BSTAR
0.000086425
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-13 07:55:25.254Z | 184.344° SSW | 2026-08-13 07:58:25.254Z | 274.358° WNW | 40.233° | 2026-08-13 08:01:25.254Z | 336.537° NNW |
| 5 mins | 2026-08-13 19:39:25.254Z | 57.441° ENE | 2026-08-13 19:41:25.254Z | 93.957° ESE | 19.825° | 2026-08-13 19:44:25.254Z | 142.853° SSE |
| 5 mins | 2026-08-13 21:15:25.254Z | 327.116° NNW | 2026-08-13 21:17:25.254Z | 278.09° WNW | 25.495° | 2026-08-13 21:20:25.254Z | 230.786° WSW |
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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