IRIDE-MS2-HEO-11, 68983
Orbit data source: Space-Track
IRIDE-MS2-HEO-11, 68983 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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68983 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: 3 days ago
TLE from 3 days ago
0 IRIDE-MS2-HEO-11
1 68983U 26100D 26315.00003471 .00028420 00000-0 26519-2 0 9996
2 68983 97.7217 209.4875 0002603 45.5607 202.9318 14.94146056 5114Epoch: 2026-11-11T00:00Z
TLE epoch observation values (Epoch: 2026-11-11T00:00:02.998Z)
Latitude
-67.36873°
Longitude
-39.55202°
Altitude
612.155 km
Speed
7.551 km/s
True Right ascension
00h 42m 27s
True Declination
-67° 14' 37"
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
21:25:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.85 km
Perigee altitude
580.227 km
Semi-major axis
6,960.176 km
Eccentricity
0.00026
Inclination
97.7217°
RAAN
209.4875°
Arg. of periapsis
45.5607°
True anomaly
202.92018°
Mean anomaly
202.9318°
Eccentric anomaly
202.92599°
Mean motion
3.73777 °/min
Orbital period
96.31 mins
BSTAR
0.0026519
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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-11 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-14 06:11:46.028Z | 5.856° NNE | 2026-11-14 06:15:46.028Z | 290.244° WNW | 64.455° | 2026-11-14 06:19:46.028Z | 203.994° SW |
| 6 mins | 2026-11-14 17:01:46.028Z | 157.462° SSE | 2026-11-14 17:04:46.028Z | 30.759° NE | 67.404° | 2026-11-14 17:07:46.028Z | 352.672° N |
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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