IRIDE-MS2-HEO-12, 68984
Orbit data source: Space-Track
IRIDE-MS2-HEO-12, 68984 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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68984 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: 15 hours ago
TLE from 15 hours ago
0 IRIDE-MS2-HEO-12
1 68984U 26100E 26265.93748528 .00000919 00000-0 98835-4 0 9997
2 68984 97.7202 161.3115 0003829 161.8561 198.2795 14.90857707 21262Epoch: 2026-09-22T22:29Z
TLE epoch observation values (Epoch: 2026-09-22T22:29:58.728Z)
Latitude
0.00003°
Longitude
-177.979°
Altitude
600.837 km
Speed
7.558 km/s
True Right ascension
10h 45m 14s
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
06:29:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.947 km
Perigee altitude
589.609 km
Semi-major axis
6,970.415 km
Eccentricity
0.00038
Inclination
97.7202°
RAAN
161.3115°
Arg. of periapsis
161.8561°
True anomaly
198.26574°
Mean anomaly
198.2795°
Eccentric anomaly
198.27262°
Mean motion
3.72954 °/min
Orbital period
96.53 mins
BSTAR
0.000098835
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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-12 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-23 16:22:07.635Z | 115.674° SE | 2026-09-23 16:24:07.635Z | 80.81° E | 24.898° | 2026-09-23 16:27:07.635Z | 22.504° NE |
| 5 mins | 2026-09-23 17:58:07.635Z | 224.15° SW | 2026-09-23 18:00:07.635Z | 264.008° W | 25.045° | 2026-09-23 18:03:07.635Z | 316.276° NNW |
| 6 mins | 2026-09-24 05:41:07.635Z | 28.907° NE | 2026-09-24 05:44:07.635Z | 107.594° ESE | 50.673° | 2026-09-24 05:47:07.635Z | 172.243° S |
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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