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: 6 hours ago
TLE from 6 hours ago
0 IRIDE-MS2-HEO-1
1 62697U 25009CS 26126.24193333 .00002421 00000-0 23093-3 0 9990
2 62697 97.7043 205.3263 0003668 125.6736 234.4827 14.94250242 71074Epoch: 2026-05-06T05:48Z
TLE epoch observation values (Epoch: 2026-05-06T05:48:23.039Z)
Latitude
0.00005°
Longitude
-105.87494°
Altitude
589.232 km
Speed
7.565 km/s
True Right ascension
13h 41m 18s
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
19:36:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.267 km
Perigee altitude
579.161 km
Semi-major axis
6,959.851 km
Eccentricity
0.00037
Inclination
97.7043°
RAAN
205.3263°
Arg. of periapsis
125.6736°
True anomaly
234.4485°
Mean anomaly
234.4827°
Eccentric anomaly
234.4656°
Mean motion
3.73803 °/min
Orbital period
96.31 mins
BSTAR
0.00023093
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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 | 2026-05-06 17:38:11.745Z | 35.724° NE | 2026-05-06 17:41:11.745Z | 104.253° ESE | 31.602° | 2026-05-06 17:44:11.745Z | 163.172° S |
| 4 mins | 2026-05-07 04:28:11.745Z | 104.22° ESE | 2026-05-07 04:30:11.745Z | 62.291° ENE | 21.956° | 2026-05-07 04:32:11.745Z | 25.74° NE |
| 5 mins | 2026-05-07 06:03:11.745Z | 222.776° SW | 2026-05-07 06:05:11.745Z | 263.813° W | 23.299° | 2026-05-07 06:08:11.745Z | 317.212° 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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