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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X41
1 62700U 25009CV 26202.16284432 .00002488 00000-0 22160-3 0 9999
2 62700 97.7058 281.1966 0000575 177.0295 183.0931 14.96936958 82492Epoch: 2026-07-21T03:54Z
TLE epoch observation values (Epoch: 2026-07-21T03:54:29.749Z)
Latitude
0.00007°
Longitude
-76.36385°
Altitude
579.817 km
Speed
7.57 km/s
True Right ascension
18h 44m 47s
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
00:00:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.776 km
Perigee altitude
572.977 km
Semi-major axis
6,951.514 km
Eccentricity
0.00006
Inclination
97.7058°
RAAN
281.1966°
Arg. of periapsis
177.0295°
True anomaly
183.09274°
Mean anomaly
183.0931°
Eccentric anomaly
183.09292°
Mean motion
3.74476 °/min
Orbital period
96.13 mins
BSTAR
0.0002216
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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 | 2026-07-21 17:19:25.243Z | 47.153° ENE | 2026-07-21 17:22:25.243Z | 97.823° ESE | 19.602° | 2026-07-21 17:24:25.243Z | 133.742° SE |
| 5 mins | 2026-07-21 18:55:25.243Z | 334.891° NNW | 2026-07-21 18:57:25.243Z | 291.99° WNW | 25.373° | 2026-07-21 19:00:25.243Z | 235.042° WSW |
| 6 mins | 2026-07-22 05:42:25.243Z | 191.659° SSW | 2026-07-22 05:45:25.243Z | 275.244° WNW | 36.361° | 2026-07-22 05:48:25.243Z | 333.001° 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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