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: 11 hours ago
TLE from 11 hours ago
0 IRIDE-MS2-HEO-1
1 62697U 25009CS 26080.97095766 .00003358 00000-0 31989-3 0 9993
2 62697 97.7076 160.9006 0000913 335.3148 24.8028 14.94050202 64315Epoch: 2026-03-21T23:18Z
TLE epoch observation values (Epoch: 2026-03-21T23:18:10.741Z)
Latitude
-0.00008°
Longitude
-8.12817°
Altitude
587.791 km
Speed
7.567 km/s
True Right ascension
10h 43m 36s
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
15:37:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.971 km
Perigee altitude
581.7 km
Semi-major axis
6,960.473 km
Eccentricity
0.00009
Inclination
97.7076°
RAAN
160.9006°
Arg. of periapsis
335.3148°
True anomaly
24.80719°
Mean anomaly
24.8028°
Eccentric anomaly
24.80499°
Mean motion
3.73753 °/min
Orbital period
96.32 mins
BSTAR
0.00031989
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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 | 2026-03-22 17:33:35.037Z | 36.045° NE | 2026-03-22 17:36:35.037Z | 92.377° ESE | 28.79° | 2026-03-22 17:39:35.037Z | 155.953° SSE |
| 4 mins | 2026-03-22 19:10:35.037Z | 317.32° NNW | 2026-03-22 19:11:35.037Z | 299.293° NW | 17.747° | 2026-03-22 19:14:35.037Z | 250.279° W |
| 4 mins | 2026-03-23 04:24:35.037Z | 91.669° ESE | 2026-03-23 04:25:35.037Z | 71.569° E | 19.978° | 2026-03-23 04:28:35.037Z | 21.285° NNE |
| 5 mins | 2026-03-23 05:58:35.037Z | 213.501° SW | 2026-03-23 06:00:35.037Z | 252.207° W | 25.438° | 2026-03-23 06:03:35.037Z | 315.575° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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