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 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-11
1 68983U 26100D 26175.19795877 .00001373 00000-0 14314-3 0 9997
2 68983 97.7376 72.5045 0005111 109.5024 250.6747 14.91379940 7743Epoch: 2026-06-24T04:45Z
TLE epoch observation values (Epoch: 2026-06-24T04:45:03.637Z)
Latitude
-0.00005°
Longitude
88.88073°
Altitude
597.855 km
Speed
7.56 km/s
True Right ascension
04h 50m 01s
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
06:06:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.212 km
Perigee altitude
587.088 km
Semi-major axis
6,968.787 km
Eccentricity
0.00051
Inclination
97.7376°
RAAN
72.5045°
Arg. of periapsis
109.5024°
True anomaly
250.61944°
Mean anomaly
250.6747°
Eccentric anomaly
250.64707°
Mean motion
3.73085 °/min
Orbital period
96.49 mins
BSTAR
0.00014314
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-25 05:28:27.459Z | 32.952° NE | 2026-06-25 05:32:27.459Z | 111.41° ESE | 28.569° | 2026-06-25 05:35:27.459Z | 161.055° S |
| 4 mins | 2026-06-25 16:20:27.459Z | 102.069° ESE | 2026-06-25 16:22:27.459Z | 62.321° ENE | 20.784° | 2026-06-25 16:24:27.459Z | 27.076° NE |
| 5 mins | 2026-06-25 17:55:27.459Z | 218.188° SW | 2026-06-25 17:57:27.459Z | 259.378° W | 25.059° | 2026-06-25 18:00:27.459Z | 317.18° 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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