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: 4 hours ago
TLE from 4 hours ago
0 IRIDE-MS2-HEO-4
1 64582U 25135BG 26290.31209513 .00001653 00000-0 16845-3 0 9996
2 64582 97.7835 43.0537 0000621 53.6404 306.4872 14.92039122 72102Epoch: 2026-10-17T07:29Z
TLE epoch observation values (Epoch: 2026-10-17T07:29:25.019Z)
Latitude
-0.00001°
Longitude
-95.12111°
Altitude
594.362 km
Speed
7.563 km/s
True Right ascension
02h 52m 12s
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
06:35:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.03 km
Perigee altitude
588.165 km
Semi-major axis
6,966.735 km
Eccentricity
0.00006
Inclination
97.7835°
RAAN
43.0537°
Arg. of periapsis
53.6404°
True anomaly
306.48148°
Mean anomaly
306.4872°
Eccentric anomaly
306.48434°
Mean motion
3.7325 °/min
Orbital period
96.45 mins
BSTAR
0.00016845
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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 | 2026-10-17 20:56:54.136Z | 348.78° N | 2026-10-17 20:58:54.136Z | 297.501° NW | 46.386° | 2026-10-17 21:02:54.136Z | 214.269° SW |
| 6 mins | 2026-10-18 07:45:54.136Z | 172.905° S | 2026-10-18 07:48:54.136Z | 294.182° NW | 75.416° | 2026-10-18 07:51:54.136Z | 343.588° 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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