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: 5 hours ago
TLE from 5 hours ago
0 IRIDE-MS2-HEO-5
1 64571U 25135AV 26120.18633238 .00002525 00000-0 24376-3 0 9993
2 64571 97.7663 235.0087 0004390 110.0481 250.1212 14.93748223 46724Epoch: 2026-04-30T04:28Z
TLE epoch observation values (Epoch: 2026-04-30T04:28:19.117Z)
Latitude
-0°
Longitude
-50.20751°
Altitude
590.346 km
Speed
7.564 km/s
True Right ascension
15h 40m 02s
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
16:38:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.333 km
Perigee altitude
580.221 km
Semi-major axis
6,961.414 km
Eccentricity
0.00044
Inclination
97.7663°
RAAN
235.0087°
Arg. of periapsis
110.0481°
True anomaly
250.0739°
Mean anomaly
250.1212°
Eccentric anomaly
250.09755°
Mean motion
3.73677 °/min
Orbital period
96.34 mins
BSTAR
0.00024376
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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 | 2026-04-30 19:31:43.341Z | 52.768° ENE | 2026-04-30 19:34:43.341Z | 101.952° ESE | 16.888° | 2026-04-30 19:36:43.341Z | 133.065° SE |
| 5 mins | 2026-04-30 21:07:43.341Z | 338.329° N | 2026-04-30 21:09:43.341Z | 291.114° WNW | 28.946° | 2026-04-30 21:12:43.341Z | 229.844° WSW |
| 6 mins | 2026-05-01 07:56:43.341Z | 191.898° SSW | 2026-05-01 07:58:43.341Z | 256.773° W | 39.592° | 2026-05-01 08:02:43.341Z | 338.446° N |
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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