IRIDE-MS2-HEO-1, 62697
Orbit data source: Space-Track
IRIDE-MS2-HEO-1, 62697 is an Italian payload satellite in SSO that was launched on Tue, 14 Jan 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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62697 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-1
1 62697U 25009CS 26171.44088378 .00001627 00000-0 15626-3 0 9994
2 62697 97.7046 249.6843 0002601 34.0995 326.0392 14.94410276 77827Epoch: 2026-06-20T10:34Z
TLE epoch observation values (Epoch: 2026-06-20T10:34:52.358Z)
Latitude
-0.00003°
Longitude
-177.68932°
Altitude
585.749 km
Speed
7.568 km/s
True Right ascension
16h 38m 44s
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
07:21:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.027 km
Perigee altitude
579.407 km
Semi-major axis
6,959.354 km
Eccentricity
0.00026
Inclination
97.7046°
RAAN
249.6843°
Arg. of periapsis
34.0995°
True anomaly
326.02255°
Mean anomaly
326.0392°
Eccentric anomaly
326.03087°
Mean motion
3.73843 °/min
Orbital period
96.3 mins
BSTAR
0.00015626
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-1 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 | 2026-06-21 04:23:56.274Z | 119.456° SE | 2026-06-21 04:26:56.274Z | 70.705° E | 21.113° | 2026-06-21 04:29:56.274Z | 19.623° NNE |
| 5 mins | 2026-06-21 05:59:56.274Z | 216.485° SW | 2026-06-21 06:01:56.274Z | 254.677° W | 24.026° | 2026-06-21 06:04:56.274Z | 314.728° NW |
| 6 mins | 2026-06-21 17:41:56.274Z | 35.968° NE | 2026-06-21 17:44:56.274Z | 119.684° SE | 33.192° | 2026-06-21 17:47:56.274Z | 169.056° 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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