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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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 26104.95019512 .00001195 00000-0 11779-3 0 9993
2 64576 97.7634 219.9977 0004120 150.6796 209.4656 14.93880917 44450Epoch: 2026-04-14T22:48Z
TLE epoch observation values (Epoch: 2026-04-14T22:48:16.858Z)
Latitude
0°
Longitude
34.80836°
Altitude
591.392 km
Speed
7.563 km/s
True Right ascension
14h 39m 59s
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
10:27:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.733 km
Perigee altitude
579.997 km
Semi-major axis
6,961.002 km
Eccentricity
0.00041
Inclination
97.7634°
RAAN
219.9977°
Arg. of periapsis
150.6796°
True anomaly
209.44239°
Mean anomaly
209.4656°
Eccentric anomaly
209.45399°
Mean motion
3.73711 °/min
Orbital period
96.33 mins
BSTAR
0.00011779
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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
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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 | 2026-04-15 06:58:49.322Z | 127.949° SE | 2026-04-15 07:01:49.322Z | 72.953° E | 26.769° | 2026-04-15 07:04:49.322Z | 14.631° NNE |
| 4 mins | 2026-04-15 08:35:49.322Z | 236.843° WSW | 2026-04-15 08:37:49.322Z | 275.245° WNW | 18.67° | 2026-04-15 08:39:49.322Z | 307.607° NW |
| 6 mins | 2026-04-15 20:16:49.322Z | 24.26° NE | 2026-04-15 20:19:49.322Z | 110.568° ESE | 40.787° | 2026-04-15 20:22:49.322Z | 178.284° S |
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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