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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS2-HEO-1
1 62697U 25009CS 26238.52753341 .00001378 00000-0 13249-3 0 9998
2 62697 97.7004 315.5226 0003601 116.4155 243.7436 14.94614197 87848Epoch: 2026-08-26T12:39Z
TLE epoch observation values (Epoch: 2026-08-26T12:39:38.886Z)
Latitude
0.00003°
Longitude
150.83132°
Altitude
587.728 km
Speed
7.566 km/s
True Right ascension
21h 02m 05s
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
11:20:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.089 km
Perigee altitude
578.077 km
Semi-major axis
6,958.72 km
Eccentricity
0.00036
Inclination
97.7004°
RAAN
315.5226°
Arg. of periapsis
116.4155°
True anomaly
243.7066°
Mean anomaly
243.7436°
Eccentric anomaly
243.7251°
Mean motion
3.73895 °/min
Orbital period
96.28 mins
BSTAR
0.00013249
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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 | 2026-08-27 04:51:47.178Z | 142.569° SSE | 2026-08-27 04:54:47.178Z | 72.913° E | 36.37° | 2026-08-27 04:57:47.178Z | 4.241° NNE |
| 6 mins | 2026-08-27 18:09:47.178Z | 9.617° NNE | 2026-08-27 18:11:47.178Z | 356.297° N | 42.916° | 2026-08-27 18:15:47.178Z | 196.232° SSW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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