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: 6 hours ago
TLE from 6 hours ago
0 IRIDE FM8
1 66702U 25276AN 26239.13289035 .00005135 00000-0 23580-3 0 9991
2 66702 97.4149 311.5508 0005461 126.2857 233.8884 15.20820791 41205Epoch: 2026-08-27T03:11Z
TLE epoch observation values (Epoch: 2026-08-27T03:11:21.726Z)
Latitude
0.00003°
Longitude
-71.66564°
Altitude
508.671 km
Speed
7.608 km/s
True Right ascension
20h 46m 12s
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
00:23:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.085 km
Perigee altitude
496.572 km
Semi-major axis
6,878.466 km
Eccentricity
0.00055
Inclination
97.4149°
RAAN
311.5508°
Arg. of periapsis
126.2857°
True anomaly
233.83787°
Mean anomaly
233.8884°
Eccentric anomaly
233.86313°
Mean motion
3.80457 °/min
Orbital period
94.62 mins
BSTAR
0.0002358
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-27 17:57:17.583Z | 5.008° NNE | 2026-08-27 18:00:17.583Z | 319.818° NNW | 40.672° | 2026-08-27 18:03:17.583Z | 205.611° SW |
| 5 mins | 2026-08-28 04:36:17.583Z | 133.723° SE | 2026-08-28 04:38:17.583Z | 66.619° ENE | 34.796° | 2026-08-28 04:41:17.583Z | 3.196° NNE |
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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