IRIDE-MS2-HEO-6, 64576
Orbit data source: Space-Track
IRIDE-MS2-HEO-6, 64576 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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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: 5 hours ago
TLE from 5 hours ago
0 IRIDE-MS2-HEO-6
1 64576U 25135BA 26036.15027352 .00004293 00000-0 41364-3 0 9995
2 64576 97.7584 152.0629 0004502 55.9367 304.2279 14.93447169 34182Epoch: 2026-02-05T03:36Z
TLE epoch observation values (Epoch: 2026-02-05T03:36:23.632Z)
Latitude
-0.00005°
Longitude
-37.34219°
Altitude
588.478 km
Speed
7.567 km/s
True Right ascension
10h 08m 15s
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
10:49:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.348 km
Perigee altitude
581.079 km
Semi-major axis
6,962.35 km
Eccentricity
0.00045
Inclination
97.7584°
RAAN
152.0629°
Arg. of periapsis
55.9367°
True anomaly
304.18523°
Mean anomaly
304.2279°
Eccentric anomaly
304.20657°
Mean motion
3.73602 °/min
Orbital period
96.36 mins
BSTAR
0.00041364
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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-6 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-05 20:14:44.397Z | 20.384° NNE | 2026-02-05 20:18:44.397Z | 101.859° ESE | 40.706° | 2026-02-05 20:22:44.397Z | 180.882° SSW |
| 5 mins | 2026-02-06 07:05:44.397Z | 122.751° SE | 2026-02-06 07:07:44.397Z | 73.842° E | 30.12° | 2026-02-06 07:10:44.397Z | 11.201° NNE |
| 4 mins | 2026-02-06 08:41:44.397Z | 239.027° WSW | 2026-02-06 08:43:44.397Z | 273.593° WNW | 16.146° | 2026-02-06 08:45:44.397Z | 304.421° NW |
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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