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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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, 1.0 m
Radar Cross Section
0.683 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IRIDE-MS2-HEO-1
1 62697U 25009CS 25259.24329842 .00002828 00000-0 27894-3 0 9996
2 62697 97.7302 337.5260 0002552 163.2997 196.8307 14.92780958 36441Epoch: 2025-09-16T05:50Z
TLE epoch observation values (Epoch: 2025-09-16T05:50:20.983Z)
Latitude
-0.00001°
Longitude
-105.49782°
Altitude
594.015 km
Speed
7.562 km/s
True Right ascension
22h 30m 06s
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
07:52:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.063 km
Perigee altitude
584.508 km
Semi-major axis
6,964.422 km
Eccentricity
0.00026
Inclination
97.7302°
RAAN
337.526°
Arg. of periapsis
163.2997°
True anomaly
196.82224°
Mean anomaly
196.8307°
Eccentric anomaly
196.82647°
Mean motion
3.73435 °/min
Orbital period
96.4 mins
BSTAR
0.00027894
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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 | 2025-09-16 17:40:39.291Z | 34.44° NE | 2025-09-16 17:43:39.291Z | 95.71° ESE | 31.313° | 2025-09-16 17:46:39.291Z | 160.598° S |
| 4 mins | 2025-09-17 04:31:39.291Z | 101.687° ESE | 2025-09-17 04:33:39.291Z | 58.84° ENE | 21.906° | 2025-09-17 04:35:39.291Z | 23.962° NE |
| 5 mins | 2025-09-17 06:06:39.291Z | 223.653° SW | 2025-09-17 06:08:39.291Z | 265.265° W | 23.469° | 2025-09-17 06:11:39.291Z | 317.709° 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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