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
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 IRIDE FM2
1 66696U 25276AG 26144.93567891 .00006978 00000-0 32641-3 0 9999
2 66696 97.4189 218.8869 0005393 95.1141 265.0709 15.20055933 26893Epoch: 2026-05-24T22:27Z
TLE epoch observation values (Epoch: 2026-05-24T22:27:22.657Z)
Latitude
-0.00012°
Longitude
-0.48817°
Altitude
509.083 km
Speed
7.609 km/s
True Right ascension
14h 35m 32s
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
13:55:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.349 km
Perigee altitude
498.927 km
Semi-major axis
6,880.775 km
Eccentricity
0.00054
Inclination
97.4189°
RAAN
218.8869°
Arg. of periapsis
95.1141°
True anomaly
265.00933°
Mean anomaly
265.0709°
Eccentric anomaly
265.04012°
Mean motion
3.80266 °/min
Orbital period
94.67 mins
BSTAR
0.00032641
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-25 04:53:36.687Z | 163.455° S | 2026-05-25 04:57:36.687Z | 10.035° NNE | 42.52° | 2026-05-25 05:00:36.687Z | 350.527° N |
| 5 mins | 2026-05-25 17:59:36.687Z | 358.452° N | 2026-05-25 18:01:36.687Z | 271.653° WNW | 41.869° | 2026-05-25 18:04:36.687Z | 204.055° SW |
| 5 mins | 2026-05-26 04:37:36.687Z | 131.856° SE | 2026-05-26 04:39:36.687Z | 57.685° ENE | 34.611° | 2026-05-26 04:42:36.687Z | 2.033° NNE |
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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