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
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIDE FM8
1 66702U 25276AN 26092.20159512 .00008492 00000-0 40713-3 0 9998
2 66702 97.4235 167.0358 0002328 286.1463 73.9515 15.19146246 18882Epoch: 2026-04-02T04:50Z
TLE epoch observation values (Epoch: 2026-04-02T04:50:17.818Z)
Latitude
-0.00004°
Longitude
-96.09191°
Altitude
511.065 km
Speed
7.609 km/s
True Right ascension
11h 08m 08s
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
03:00:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.99 km
Perigee altitude
503.785 km
Semi-major axis
6,883.524 km
Eccentricity
0.00023
Inclination
97.4235°
RAAN
167.0358°
Arg. of periapsis
286.1463°
True anomaly
73.97714°
Mean anomaly
73.9515°
Eccentric anomaly
73.96432°
Mean motion
3.80038 °/min
Orbital period
94.73 mins
BSTAR
0.00040713
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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 | 2026-04-03 04:40:39.312Z | 149.353° SSE | 2026-04-03 04:43:39.312Z | 87.613° E | 37.727° | 2026-04-03 04:46:39.312Z | 2.052° NNE |
| 5 mins | 2026-04-03 17:46:39.312Z | 15.565° NNE | 2026-04-03 17:48:39.312Z | 103.804° ESE | 44.793° | 2026-04-03 17:51:39.312Z | 190.02° SSW |
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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