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: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-5
1 64571U 25135AV 26289.92081410 .00001777 00000-0 18071-3 0 9993
2 64571 97.7835 42.4988 0000735 58.5406 301.5885 14.92041580 72038Epoch: 2026-10-16T22:05Z
TLE epoch observation values (Epoch: 2026-10-16T22:05:58.338Z)
Latitude
0.00003°
Longitude
45.57082°
Altitude
594.344 km
Speed
7.563 km/s
True Right ascension
02h 49m 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
03:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.102 km
Perigee altitude
588.078 km
Semi-major axis
6,966.727 km
Eccentricity
0.00007
Inclination
97.7835°
RAAN
42.4988°
Arg. of periapsis
58.5406°
True anomaly
301.58133°
Mean anomaly
301.5885°
Eccentric anomaly
301.58491°
Mean motion
3.7325 °/min
Orbital period
96.45 mins
BSTAR
0.00018071
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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 | 2026-10-17 19:36:38.998Z | 50.624° ENE | 2026-10-17 19:39:38.998Z | 101.785° ESE | 20.142° | 2026-10-17 19:41:38.998Z | 134.875° SE |
| 5 mins | 2026-10-17 21:12:38.998Z | 337.422° NNW | 2026-10-17 21:14:38.998Z | 295.072° NW | 30.553° | 2026-10-17 21:17:38.998Z | 234.65° WSW |
| 6 mins | 2026-10-18 08:01:38.998Z | 190.857° SSW | 2026-10-18 08:04:38.998Z | 267.022° W | 48.584° | 2026-10-18 08:07:38.998Z | 331.696° NNW |
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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