ICEYE-X41, 62700
Orbit data source: Space-Track
ICEYE-X41, 62700 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Tue, 14 Jan 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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62700 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.6 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X41
1 62700U 25009CV 25286.49206884 .00006444 00000-0 60137-3 0 9993
2 62700 97.7283 4.6939 0002711 118.5955 241.5538 14.94533332 40536Epoch: 2025-10-13T11:48Z
TLE epoch observation values (Epoch: 2025-10-13T11:48:34.747Z)
Latitude
-0.00008°
Longitude
165.25506°
Altitude
587.768 km
Speed
7.566 km/s
True Right ascension
00h 18m 46s
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
18:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.722 km
Perigee altitude
578.949 km
Semi-major axis
6,958.972 km
Eccentricity
0.00027
Inclination
97.7283°
RAAN
4.6939°
Arg. of periapsis
118.5955°
True anomaly
241.52649°
Mean anomaly
241.5538°
Eccentric anomaly
241.54014°
Mean motion
3.73874 °/min
Orbital period
96.29 mins
BSTAR
0.00060137
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.ICEYE-X41 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 | 2025-10-14 05:36:54.707Z | 184.671° SSW | 2025-10-14 05:39:54.707Z | 274.068° WNW | 39.995° | 2025-10-14 05:42:54.707Z | 336.432° NNW |
| 4 mins | 2025-10-14 17:19:54.707Z | 60.36° ENE | 2025-10-14 17:21:54.707Z | 97.937° ESE | 19.285° | 2025-10-14 17:23:54.707Z | 133.171° SE |
| 5 mins | 2025-10-14 18:54:54.707Z | 337.334° NNW | 2025-10-14 18:56:54.707Z | 296.022° NW | 25.944° | 2025-10-14 18:59:54.707Z | 235.71° WSW |
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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