IRIDE FM6, 66700
Orbit data source: Space-Track
IRIDE FM6, 66700 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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66700 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: 1 day ago
TLE from 1 day ago
0 IRIDE FM6
1 66700U 25276AL 26063.16307091 .00014973 00000-0 70393-3 0 9994
2 66700 97.4302 138.6483 0000988 7.0516 353.0733 15.19681606 14487Epoch: 2026-03-04T03:54Z
TLE epoch observation values (Epoch: 2026-03-04T03:54:49.326Z)
Latitude
0.00001°
Longitude
-81.98895°
Altitude
509.216 km
Speed
7.61 km/s
True Right ascension
09h 14m 35s
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
09:06:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.449 km
Perigee altitude
503.089 km
Semi-major axis
6,881.906 km
Eccentricity
0.0001
Inclination
97.4302°
RAAN
138.6483°
Arg. of periapsis
7.0516°
True anomaly
353.07193°
Mean anomaly
353.0733°
Eccentric anomaly
353.07262°
Mean motion
3.80172 °/min
Orbital period
94.69 mins
BSTAR
0.00070393
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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 FM6 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 | 2026-03-05 05:19:12.163Z | 187.787° SSW | 2026-03-05 05:22:12.163Z | 256.414° W | 36.253° | 2026-03-05 05:25:12.163Z | 332.65° NNW |
| 4 mins | 2026-03-05 18:25:12.163Z | 329.716° NNW | 2026-03-05 18:26:12.163Z | 304.417° NW | 26.433° | 2026-03-05 18:29:12.163Z | 231.837° WSW |
| 6 mins | 2026-03-06 05:02:12.163Z | 170.127° S | 2026-03-06 05:04:12.163Z | 181.953° SSW | 42.594° | 2026-03-06 05:08:12.163Z | 346.643° N |
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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