IRIDE-MS2-HEO-14, 68986
Orbit data source: Space-Track
IRIDE-MS2-HEO-14, 68986 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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68986 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 9 hours ago
TLE from 9 hours ago
0 IRIDE-MS2-HEO-14
1 68986U 26100G 26168.67592750 .00000925 00000-0 97108-4 0 9995
2 68986 97.7365 66.1277 0003039 104.0341 256.1216 14.91825333 6775Epoch: 2026-06-17T16:13Z
TLE epoch observation values (Epoch: 2026-06-17T16:13:20.135Z)
Latitude
-0.00004°
Longitude
-83.13639°
Altitude
595.795 km
Speed
7.562 km/s
True Right ascension
04h 24m 30s
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
12:06:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.379 km
Perigee altitude
587.144 km
Semi-major axis
6,967.399 km
Eccentricity
0.0003
Inclination
97.7365°
RAAN
66.1277°
Arg. of periapsis
104.0341°
True anomaly
256.0878°
Mean anomaly
256.1216°
Eccentric anomaly
256.1047°
Mean motion
3.73196 °/min
Orbital period
96.46 mins
BSTAR
0.000097108
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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-14 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 | 2026-06-18 05:40:33.853Z | 29.466° NE | 2026-06-18 05:43:33.853Z | 93.985° ESE | 35.795° | 2026-06-18 05:47:33.853Z | 173.107° S |
| 5 mins | 2026-06-18 16:31:33.853Z | 113.791° SE | 2026-06-18 16:33:33.853Z | 68.977° E | 26.028° | 2026-06-18 16:36:33.853Z | 14.338° NNE |
| 4 mins | 2026-06-18 18:07:33.853Z | 236.228° WSW | 2026-06-18 18:09:33.853Z | 275.682° WNW | 19.449° | 2026-06-18 18:11:33.853Z | 308.431° 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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