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 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-12
1 68984U 26100E 26175.20483421 .00001308 00000-0 13721-3 0 9998
2 68984 97.7336 72.4726 0005465 119.6454 240.5309 14.91185759 7741Epoch: 2026-06-24T04:54Z
TLE epoch observation values (Epoch: 2026-06-24T04:54:57.675Z)
Latitude
-0.00008°
Longitude
86.3669°
Altitude
599.155 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
06:05:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.064 km
Perigee altitude
587.447 km
Semi-major axis
6,969.393 km
Eccentricity
0.00055
Inclination
97.7336°
RAAN
72.4726°
Arg. of periapsis
119.6454°
True anomaly
240.4764°
Mean anomaly
240.5309°
Eccentric anomaly
240.50365°
Mean motion
3.73036 °/min
Orbital period
96.51 mins
BSTAR
0.00013721
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-25 05:38:26.985Z | 27.414° NE | 2026-06-25 05:42:26.985Z | 117.2° SE | 34.352° | 2026-06-25 05:45:26.985Z | 169.63° S |
| 5 mins | 2026-06-25 16:30:26.985Z | 109.474° ESE | 2026-06-25 16:32:26.985Z | 62.723° ENE | 25.425° | 2026-06-25 16:35:26.985Z | 12.889° NNE |
| 4 mins | 2026-06-25 18:06:26.985Z | 239.033° WSW | 2026-06-25 18:07:26.985Z | 258.638° W | 20.126° | 2026-06-25 18:10:26.985Z | 311.056° 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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