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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X41
1 62700U 25009CV 26256.16812538 .00002851 00000-0 25145-3 0 9992
2 62700 97.7016 334.4150 0003371 94.7245 265.4362 14.97205616 90572Epoch: 2026-09-13T04:02Z
TLE epoch observation values (Epoch: 2026-09-13T04:02:06.032Z)
Latitude
-0.00004°
Longitude
-78.27678°
Altitude
578.773 km
Speed
7.571 km/s
True Right ascension
22h 17m 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
02:48:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.887 km
Perigee altitude
570.201 km
Semi-major axis
6,950.681 km
Eccentricity
0.00034
Inclination
97.7016°
RAAN
334.415°
Arg. of periapsis
94.7245°
True anomaly
265.39769°
Mean anomaly
265.4362°
Eccentric anomaly
265.41695°
Mean motion
3.74543 °/min
Orbital period
96.12 mins
BSTAR
0.00025145
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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 | 2026-09-13 17:26:29.714Z | 40.605° NE | 2026-09-13 17:29:29.714Z | 90.698° ESE | 25.259° | 2026-09-13 17:32:29.714Z | 146.966° SSE |
| 4 mins | 2026-09-13 19:03:29.714Z | 319.511° NNW | 2026-09-13 19:04:29.714Z | 298.494° NW | 23.494° | 2026-09-13 19:07:29.714Z | 243.092° WSW |
| 5 mins | 2026-09-14 05:50:29.714Z | 208.831° SW | 2026-09-14 05:52:29.714Z | 266.295° W | 39.429° | 2026-09-14 05:55:29.714Z | 327.477° NNW |
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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