IRIDE FM8, 66702
Orbit data source: Space-Track
IRIDE FM8, 66702 is an Italian payload satellite in SSO that was launched on Fri, 28 Nov 2025 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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66702 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 IRIDE FM8
1 66702U 25276AN 26192.73986039 .00003197 00000-0 15008-3 0 9995
2 66702 97.4188 265.9002 0002432 310.9219 49.1806 15.20351070 34155Epoch: 2026-07-11T17:45Z
TLE epoch observation values (Epoch: 2026-07-11T17:45:23.937Z)
Latitude
0.00002°
Longitude
69.90171°
Altitude
506.777 km
Speed
7.611 km/s
True Right ascension
17h 43m 36s
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
17:11:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.42 km
Perigee altitude
500.074 km
Semi-major axis
6,879.884 km
Eccentricity
0.00024
Inclination
97.4188°
RAAN
265.9002°
Arg. of periapsis
310.9219°
True anomaly
49.20169°
Mean anomaly
49.1806°
Eccentric anomaly
49.19115°
Mean motion
3.8034 °/min
Orbital period
94.65 mins
BSTAR
0.00015008
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Other satellites on launch #276 in the year 2025 (2025-11-28 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 FM8 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 | 2026-07-12 04:55:46.542Z | 165.952° S | 2026-07-12 04:59:46.542Z | 356.039° N | 43.527° | 2026-07-12 05:02:46.542Z | 348.81° N |
| 5 mins | 2026-07-12 18:01:46.542Z | 355.04° N | 2026-07-12 18:03:46.542Z | 271.071° WNW | 40.433° | 2026-07-12 18:06:46.542Z | 206.511° SW |
| 6 mins | 2026-07-13 04:38:46.542Z | 143.537° SSE | 2026-07-13 04:40:46.542Z | 102.07° ESE | 35.185° | 2026-07-13 04:44:46.542Z | 359.801° N |
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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