IRIDE-MS2-HEO-5, 64571
Orbit data source: Space-Track
IRIDE-MS2-HEO-5, 64571 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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64571 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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS2-HEO-5
1 64571U 25135AV 26171.54812179 .00001314 00000-0 13526-3 0 9992
2 64571 97.7731 285.6783 0000912 48.6897 311.4400 14.91957524 54382Epoch: 2026-06-20T13:09Z
TLE epoch observation values (Epoch: 2026-06-20T13:09:17.722Z)
Latitude
-0.00006°
Longitude
179.5933°
Altitude
594.453 km
Speed
7.563 km/s
True Right ascension
19h 02m 42s
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
07:19:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.487 km
Perigee altitude
588.216 km
Semi-major axis
6,966.989 km
Eccentricity
0.00009
Inclination
97.7731°
RAAN
285.6783°
Arg. of periapsis
48.6897°
True anomaly
311.43217°
Mean anomaly
311.44°
Eccentric anomaly
311.43608°
Mean motion
3.73229 °/min
Orbital period
96.46 mins
BSTAR
0.00013526
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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-5 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 07:00:53.092Z | 118.27° SE | 2026-06-21 07:02:53.092Z | 73.926° E | 27.39° | 2026-06-21 07:05:53.092Z | 14.406° NNE |
| 4 mins | 2026-06-21 08:36:53.092Z | 235.012° WSW | 2026-06-21 08:38:53.092Z | 272.048° WNW | 18.523° | 2026-06-21 08:40:53.092Z | 305.229° NW |
| 5 mins | 2026-06-21 20:18:53.092Z | 22.531° NE | 2026-06-21 20:21:53.092Z | 107.278° ESE | 41.881° | 2026-06-21 20:23:53.092Z | 174.533° 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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