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 spacecraft
Bus & Motor
HAWK, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 IRIDE-MS2-HEO-10
1 68982U 26100C 26175.20284440 .00001335 00000-0 13999-3 0 9993
2 68982 97.7331 72.4719 0005447 121.2112 238.9641 14.91173623 7743Epoch: 2026-06-24T04:52Z
TLE epoch observation values (Epoch: 2026-06-24T04:52:05.756Z)
Latitude
0°
Longitude
87.08448°
Altitude
599.277 km
Speed
7.559 km/s
True Right ascension
04h 49m 53s
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
06:03:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.09 km
Perigee altitude
587.497 km
Semi-major axis
6,969.43 km
Eccentricity
0.00054
Inclination
97.7331°
RAAN
72.4719°
Arg. of periapsis
121.2112°
True anomaly
238.91064°
Mean anomaly
238.9641°
Eccentric anomaly
238.93737°
Mean motion
3.73033 °/min
Orbital period
96.51 mins
BSTAR
0.00013999
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-25 05:36:06.827Z | 32.15° NE | 2026-06-25 05:39:06.827Z | 94.689° ESE | 33.39° | 2026-06-25 05:43:06.827Z | 169.832° S |
| 5 mins | 2026-06-25 16:27:06.827Z | 114.981° SE | 2026-06-25 16:29:06.827Z | 76.389° E | 24.098° | 2026-06-25 16:32:06.827Z | 18.971° NNE |
| 5 mins | 2026-06-25 18:03:06.827Z | 228.965° WSW | 2026-06-25 18:05:06.827Z | 269.079° W | 21.494° | 2026-06-25 18:08:06.827Z | 317.213° 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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