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
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-14
1 68986U 26100G 26265.94251648 .00000911 00000-0 96410-4 0 9991
2 68986 97.7223 161.4931 0004392 119.3314 240.8344 14.91523444 21278Epoch: 2026-09-22T22:37Z
TLE epoch observation values (Epoch: 2026-09-22T22:37:13.423Z)
Latitude
-0.00004°
Longitude
-179.61358°
Altitude
597.721 km
Speed
7.56 km/s
True Right ascension
10h 45m 58s
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
06:29:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.263 km
Perigee altitude
587.142 km
Semi-major axis
6,968.339 km
Eccentricity
0.00044
Inclination
97.7223°
RAAN
161.4931°
Arg. of periapsis
119.3314°
True anomaly
240.79046°
Mean anomaly
240.8344°
Eccentric anomaly
240.81243°
Mean motion
3.73121 °/min
Orbital period
96.48 mins
BSTAR
0.00009641
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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 | 2026-09-23 16:27:52.092Z | 128.825° SE | 2026-09-23 16:30:52.092Z | 81.049° E | 28.668° | 2026-09-23 16:34:52.092Z | 10.262° NNE |
| 5 mins | 2026-09-23 18:04:52.092Z | 229.085° WSW | 2026-09-23 18:06:52.092Z | 266.074° W | 21.467° | 2026-09-23 18:09:52.092Z | 314.38° NW |
| 6 mins | 2026-09-24 05:47:52.092Z | 26.973° NE | 2026-09-24 05:49:52.092Z | 69.062° E | 55.581° | 2026-09-24 05:53:52.092Z | 179.433° S |
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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