IRIDE-MS2-HEO-15, 68987
Orbit data source: Space-Track
IRIDE-MS2-HEO-15, 68987 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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68987 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: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-15
1 68987U 26100H 26266.12804866 .00001070 00000-0 11093-3 0 9999
2 68987 97.7199 161.6706 0002395 126.1872 233.9569 14.92025393 21306Epoch: 2026-09-23T03:04Z
TLE epoch observation values (Epoch: 2026-09-23T03:04:23.404Z)
Latitude
0.00002°
Longitude
113.58946°
Altitude
595.647 km
Speed
7.561 km/s
True Right ascension
10h 46m 40s
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
06:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.306 km
Perigee altitude
586.969 km
Semi-major axis
6,966.775 km
Eccentricity
0.00024
Inclination
97.7199°
RAAN
161.6706°
Arg. of periapsis
126.1872°
True anomaly
233.93471°
Mean anomaly
233.9569°
Eccentric anomaly
233.94581°
Mean motion
3.73246 °/min
Orbital period
96.45 mins
BSTAR
0.00011093
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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-15 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-23 16:06:31.859Z | 102.092° ESE | 2026-09-23 16:08:31.859Z | 71.005° E | 17.121° | 2026-09-23 16:10:31.859Z | 37.357° NE |
| 6 mins | 2026-09-23 17:41:31.859Z | 203.256° SW | 2026-09-23 17:43:31.859Z | 244.185° WSW | 36.736° | 2026-09-23 17:47:31.859Z | 328.892° NNW |
| 5 mins | 2026-09-24 05:25:31.859Z | 53.301° ENE | 2026-09-24 05:27:31.859Z | 102.857° ESE | 31.567° | 2026-09-24 05:30:31.859Z | 156.914° SSE |
| 4 mins | 2026-09-24 07:01:31.859Z | 314.407° NW | 2026-09-24 07:02:31.859Z | 295.237° NW | 20.154° | 2026-09-24 07:05:31.859Z | 246.867° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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