IRIDE FM1, 66695
Orbit data source: Space-Track
IRIDE FM1, 66695 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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66695 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 FM1
1 66695U 25276AF 26147.15454289 .00006838 00000-0 31509-3 0 9998
2 66695 97.4204 221.2944 0002098 76.0150 284.1318 15.20595841 27244Epoch: 2026-05-27T03:42Z
TLE epoch observation values (Epoch: 2026-05-27T03:42:32.505Z)
Latitude
-0.0001°
Longitude
-79.05872°
Altitude
506.781 km
Speed
7.611 km/s
True Right ascension
14h 45m 10s
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
04:47:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.451 km
Perigee altitude
499.565 km
Semi-major axis
6,879.145 km
Eccentricity
0.00021
Inclination
97.4204°
RAAN
221.2944°
Arg. of periapsis
76.015°
True anomaly
284.10848°
Mean anomaly
284.1318°
Eccentric anomaly
284.12014°
Mean motion
3.80401 °/min
Orbital period
94.64 mins
BSTAR
0.00031509
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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 FM1 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 | 2026-05-28 05:06:32.234Z | 175.989° S | 2026-05-28 05:09:32.234Z | 301.447° NW | 42.279° | 2026-05-28 05:12:32.234Z | 343.093° N |
| 6 mins | 2026-05-28 18:10:32.234Z | 354.373° N | 2026-05-28 18:13:32.234Z | 269.534° W | 34.706° | 2026-05-28 18:16:32.234Z | 213.774° 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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