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 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: 15 hours ago
TLE from 15 hours ago
0 IRIDE-MS2-HEO-15
1 68987U 26100H 26175.18297229 .00001286 00000-0 13289-3 0 9991
2 68987 97.7336 72.4990 0003128 97.2141 262.9433 14.91821951 7742Epoch: 2026-06-24T04:23Z
TLE epoch observation values (Epoch: 2026-06-24T04:23:28.805Z)
Latitude
-0.0001°
Longitude
94.28515°
Altitude
595.566 km
Speed
7.562 km/s
True Right ascension
04h 49m 59s
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
06:04:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.452 km
Perigee altitude
587.093 km
Semi-major axis
6,967.409 km
Eccentricity
0.00031
Inclination
97.7336°
RAAN
72.499°
Arg. of periapsis
97.2141°
True anomaly
262.90773°
Mean anomaly
262.9433°
Eccentric anomaly
262.92551°
Mean motion
3.73195 °/min
Orbital period
96.46 mins
BSTAR
0.00013289
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-25 05:07:33.917Z | 51.891° ENE | 2026-06-25 05:10:33.917Z | 102.836° ESE | 18.213° | 2026-06-25 05:12:33.917Z | 134.848° SE |
| 5 mins | 2026-06-25 06:43:33.917Z | 337.648° N | 2026-06-25 06:45:33.917Z | 293.857° NW | 27.528° | 2026-06-25 06:48:33.917Z | 233.07° WSW |
| 6 mins | 2026-06-25 17:32:33.917Z | 188.796° SSW | 2026-06-25 17:35:33.917Z | 261.73° W | 37.682° | 2026-06-25 17:38:33.917Z | 332.111° 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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