IRIDE FM2, 66696
Orbit data source: Space-Track
IRIDE FM2, 66696 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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66696 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: 7 hours ago
TLE from 7 hours ago
0 IRIDE FM2
1 66696U 25276AG 26192.78096317 .00004075 00000-0 18800-3 0 9992
2 66696 97.4181 265.9702 0001913 277.2708 82.8310 15.20796838 34168Epoch: 2026-07-11T18:44Z
TLE epoch observation values (Epoch: 2026-07-11T18:44:35.217Z)
Latitude
-0.00005°
Longitude
55.13421°
Altitude
506.363 km
Speed
7.611 km/s
True Right ascension
17h 43m 52s
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
14:31:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.717 km
Perigee altitude
499.085 km
Semi-major axis
6,878.538 km
Eccentricity
0.00019
Inclination
97.4181°
RAAN
265.9702°
Arg. of periapsis
277.2708°
True anomaly
82.85275°
Mean anomaly
82.831°
Eccentric anomaly
82.84188°
Mean motion
3.80451 °/min
Orbital period
94.62 mins
BSTAR
0.000188
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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 FM2 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 | 2026-07-12 04:21:34.479Z | 126.928° SE | 2026-07-12 04:24:34.479Z | 57.978° ENE | 25.361° | 2026-07-12 04:26:34.479Z | 17.813° NNE |
| 5 mins | 2026-07-12 17:25:34.479Z | 33.11° NE | 2026-07-12 17:27:34.479Z | 77.912° E | 33.41° | 2026-07-12 17:30:34.479Z | 166.016° S |
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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