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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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: 6 hours ago
TLE from 6 hours ago
0 IRIDE-MS2-HEO-5
1 64571U 25135AV 25328.52333280 .00003279 00000-0 32283-3 0 9997
2 64571 97.7586 80.3991 0001507 273.6547 86.4500 14.92751343 23348Epoch: 2025-11-24T12:33Z
TLE epoch observation values (Epoch: 2025-11-24T12:33:35.953Z)
Latitude
-0.00004°
Longitude
-171.72278°
Altitude
592.339 km
Speed
7.564 km/s
True Right ascension
05h 21m 35s
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
16:05:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.428 km
Perigee altitude
585.329 km
Semi-major axis
6,964.516 km
Eccentricity
0.00015
Inclination
97.7586°
RAAN
80.3991°
Arg. of periapsis
273.6547°
True anomaly
86.46724°
Mean anomaly
86.45°
Eccentric anomaly
86.45862°
Mean motion
3.73428 °/min
Orbital period
96.4 mins
BSTAR
0.00032283
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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 | 2025-11-24 19:34:45.514Z | 48.849° ENE | 2025-11-24 19:37:45.514Z | 98.46° ESE | 18.912° | 2025-11-24 19:39:45.514Z | 132.741° SE |
| 5 mins | 2025-11-24 21:10:45.514Z | 339.089° N | 2025-11-24 21:12:45.514Z | 298.552° NW | 26.714° | 2025-11-24 21:15:45.514Z | 235.626° WSW |
| 6 mins | 2025-11-25 07:59:45.514Z | 191.427° SSW | 2025-11-25 08:02:45.514Z | 274.84° WNW | 36.737° | 2025-11-25 08:05:45.514Z | 332.927° 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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