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: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-13
1 68985U 26100F 26168.67853374 .00001183 00000-0 12295-3 0 9996
2 68985 97.7368 66.1279 0003486 107.5048 252.6552 14.91740707 6772Epoch: 2026-06-17T16:17Z
TLE epoch observation values (Epoch: 2026-06-17T16:17:05.315Z)
Latitude
-0°
Longitude
-84.07701°
Altitude
596.275 km
Speed
7.561 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
12:50:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.955 km
Perigee altitude
587.097 km
Semi-major axis
6,967.663 km
Eccentricity
0.00035
Inclination
97.7368°
RAAN
66.1279°
Arg. of periapsis
107.5048°
True anomaly
252.61707°
Mean anomaly
252.6552°
Eccentric anomaly
252.63614°
Mean motion
3.73175 °/min
Orbital period
96.47 mins
BSTAR
0.00012295
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-18 05:44:23.934Z | 27.351° NE | 2026-06-18 05:47:23.934Z | 97.555° ESE | 38.048° | 2026-06-18 05:51:23.934Z | 176.523° S |
| 5 mins | 2026-06-18 16:35:23.934Z | 116.121° SE | 2026-06-18 16:37:23.934Z | 67.534° E | 27.955° | 2026-06-18 16:40:23.934Z | 12.042° NNE |
| 4 mins | 2026-06-18 18:11:23.934Z | 238.608° WSW | 2026-06-18 18:13:23.934Z | 275.783° WNW | 17.881° | 2026-06-18 18:15:23.934Z | 307.169° 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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