IRIDE-MS2-HEO-13, 68985
AKA "IRIDE-MS2-HEO-13" on Space-Track | Orbit data source: Space-Track
IRIDE-MS2-HEO-13, 68985 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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68985 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: 21 hours ago
TLE from 21 hours ago
0 IRIDE-MS2-HEO-13
1 68985U 26100F 26174.98376411 .00001241 00000-0 12871-3 0 9994
2 68985 97.7366 72.3158 0003668 95.4778 264.6860 14.91755438 7719Epoch: 2026-06-23T23:36Z
TLE epoch observation values (Epoch: 2026-06-23T23:36:37.219Z)
Latitude
0.00007°
Longitude
166.01321°
Altitude
595.742 km
Speed
7.562 km/s
True Right ascension
04h 49m 15s
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
07:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.035 km
Perigee altitude
586.924 km
Semi-major axis
6,967.617 km
Eccentricity
0.00037
Inclination
97.7366°
RAAN
72.3158°
Arg. of periapsis
95.4778°
True anomaly
264.64415°
Mean anomaly
264.686°
Eccentric anomaly
264.66507°
Mean motion
3.73179 °/min
Orbital period
96.47 mins
BSTAR
0.00012871
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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-13 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-25 05:10:13.168Z | 47.476° ENE | 2026-06-25 05:13:13.168Z | 97.357° ESE | 19.673° | 2026-06-25 05:16:13.168Z | 144.171° SSE |
| 6 mins | 2026-06-25 06:46:13.168Z | 339.542° N | 2026-06-25 06:48:13.168Z | 301.524° NW | 25.665° | 2026-06-25 06:52:13.168Z | 229.477° WSW |
| 6 mins | 2026-06-25 17:36:13.168Z | 197.419° SSW | 2026-06-25 17:38:13.168Z | 246.321° WSW | 35.516° | 2026-06-25 17:42:13.168Z | 333.904° NNW |
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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