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 26104.95221554 .00001657 00000-0 15148-3 0 9998
2 62700 97.7072 185.4166 0001313 179.6448 180.4775 14.96344585 67955Epoch: 2026-04-14T22:51Z
TLE epoch observation values (Epoch: 2026-04-14T22:51:11.422Z)
Latitude
0.00001°
Longitude
-0.50208°
Altitude
582.165 km
Speed
7.569 km/s
True Right ascension
12h 21m 39s
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
15:48:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.126 km
Perigee altitude
574.3 km
Semi-major axis
6,953.35 km
Eccentricity
0.00013
Inclination
97.7072°
RAAN
185.4166°
Arg. of periapsis
179.6448°
True anomaly
180.47737°
Mean anomaly
180.4775°
Eccentric anomaly
180.47744°
Mean motion
3.74328 °/min
Orbital period
96.17 mins
BSTAR
0.00015148
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-15 18:41:36.990Z | 343.197° N | 2026-04-15 18:43:36.990Z | 289.521° WNW | 33.103° | 2026-04-15 18:46:36.990Z | 222.777° SW |
| 6 mins | 2026-04-16 05:28:36.990Z | 175.579° S | 2026-04-16 05:31:36.990Z | 280.372° WNW | 43.493° | 2026-04-16 05:34:36.990Z | 341.914° N |
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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