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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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: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X41
1 62700U 25009CV 26048.77256648 .00004134 00000-0 37453-3 0 9993
2 62700 97.7154 130.0804 0002952 81.0165 279.1391 14.95906340 59552Epoch: 2026-02-17T18:32Z
TLE epoch observation values (Epoch: 2026-02-17T18:32:29.743Z)
Latitude
0.00003°
Longitude
64.2087°
Altitude
582.284 km
Speed
7.569 km/s
True Right ascension
08h 40m 19s
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
07:11:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.625 km
Perigee altitude
574.519 km
Semi-major axis
6,954.709 km
Eccentricity
0.0003
Inclination
97.7154°
RAAN
130.0804°
Arg. of periapsis
81.0165°
True anomaly
279.1057°
Mean anomaly
279.1391°
Eccentric anomaly
279.1224°
Mean motion
3.74218 °/min
Orbital period
96.2 mins
BSTAR
0.00037453
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-18 04:20:05.628Z | 101.639° ESE | 2026-02-18 04:22:05.628Z | 68.341° E | 16.972° | 2026-02-18 04:24:05.628Z | 34.201° NE |
| 5 mins | 2026-02-18 05:55:05.628Z | 210.392° SW | 2026-02-18 05:57:05.628Z | 258.481° W | 29.711° | 2026-02-18 06:00:05.628Z | 322.813° NNW |
| 6 mins | 2026-02-18 17:36:05.628Z | 42.665° NE | 2026-02-18 17:39:05.628Z | 110.374° ESE | 27.107° | 2026-02-18 17:42:05.628Z | 159.42° S |
| 4 mins | 2026-02-18 19:12:05.628Z | 322.671° NNW | 2026-02-18 19:14:05.628Z | 285.322° WNW | 18.219° | 2026-02-18 19:16:05.628Z | 252.603° W |
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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