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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 IRIDE FM2
1 66696U 25276AG 26034.15514047 .00011026 00000-0 54135-3 0 9998
2 66696 97.4323 109.9824 0005029 116.8522 243.3227 15.18237175 10078Epoch: 2026-02-03T03:43Z
TLE epoch observation values (Epoch: 2026-02-03T03:43:24.136Z)
Latitude
-0°
Longitude
-79.2083°
Altitude
515.813 km
Speed
7.605 km/s
True Right ascension
07h 19m 55s
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
05:36:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.601 km
Perigee altitude
504.674 km
Semi-major axis
6,886.275 km
Eccentricity
0.0005
Inclination
97.4323°
RAAN
109.9824°
Arg. of periapsis
116.8522°
True anomaly
243.27122°
Mean anomaly
243.3227°
Eccentric anomaly
243.29696°
Mean motion
3.7981 °/min
Orbital period
94.78 mins
BSTAR
0.00054135
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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 05:09:17.619Z | 177.918° S | 2026-02-04 05:12:17.619Z | 247.39° WSW | 42.074° | 2026-02-04 05:15:17.619Z | 339.65° N |
| 5 mins | 2026-02-04 18:15:17.619Z | 347.982° N | 2026-02-04 18:17:17.619Z | 300.225° NW | 32.272° | 2026-02-04 18:20:17.619Z | 221.627° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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