IRIDE-MS2-HEO-10, 68982
Orbit data source: Space-Track
IRIDE-MS2-HEO-10, 68982 is an Italian payload satellite in SSO that was launched on Sun, 03 May 2026 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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68982 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: 16 hours ago
TLE from 16 hours ago
0 IRIDE-MS2-HEO-10
1 68982U 26100C 26237.53792884 .00001267 00000-0 13270-3 0 9990
2 68982 97.7236 133.5401 0002857 298.8713 61.2219 14.91322901 17030Epoch: 2026-08-25T12:54Z
TLE epoch observation values (Epoch: 2026-08-25T12:54:37.051Z)
Latitude
-0.00002°
Longitude
-33.91812°
Altitude
595.893 km
Speed
7.562 km/s
True Right ascension
08h 54m 09s
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
19:44:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.818 km
Perigee altitude
588.836 km
Semi-major axis
6,968.964 km
Eccentricity
0.00029
Inclination
97.7236°
RAAN
133.5401°
Arg. of periapsis
298.8713°
True anomaly
61.2506°
Mean anomaly
61.2219°
Eccentric anomaly
61.23625°
Mean motion
3.7307 °/min
Orbital period
96.5 mins
BSTAR
0.0001327
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Other satellites on launch #100 in the year 2026 (2026-05-03 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-10 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 | 2026-08-26 05:35:32.078Z | 32.488° NE | 2026-08-26 05:38:32.078Z | 99.445° ESE | 34.03° | 2026-08-26 05:41:32.078Z | 165.177° S |
| 5 mins | 2026-08-26 16:26:32.078Z | 112.597° SE | 2026-08-26 16:28:32.078Z | 70.993° E | 24.593° | 2026-08-26 16:31:32.078Z | 16.589° NNE |
| 4 mins | 2026-08-26 18:02:32.078Z | 232.874° WSW | 2026-08-26 18:04:32.078Z | 273.954° WNW | 21.012° | 2026-08-26 18:06:32.078Z | 308.616° NW |
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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