ICEYE-X44, 62707
Orbit data source: Space-Track
ICEYE-X44, 62707 is an Emirian payload satellite 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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62707 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / UAERelated business
None
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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X44
1 62707U 25009DC 25339.96830815 .00007471 00000-0 69604-3 0 9997
2 62707 97.7244 57.1919 0002525 75.5408 284.6092 14.94544943 71064Epoch: 2025-12-05T23:14Z
TLE epoch observation values (Epoch: 2025-12-05T23:14:21.824Z)
Latitude
-0.00005°
Longitude
-6.40182°
Altitude
586.389 km
Speed
7.567 km/s
True Right ascension
03h 48m 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
05:48:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.556 km
Perigee altitude
579.042 km
Semi-major axis
6,958.936 km
Eccentricity
0.00025
Inclination
97.7244°
RAAN
57.1919°
Arg. of periapsis
75.5408°
True anomaly
284.5812°
Mean anomaly
284.6092°
Eccentric anomaly
284.5952°
Mean motion
3.73877 °/min
Orbital period
96.29 mins
BSTAR
0.00069604
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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-X44 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 | 2025-12-06 17:29:24.656Z | 39.536° NE | 2025-12-06 17:32:24.656Z | 91.524° ESE | 24.774° | 2025-12-06 17:35:24.656Z | 149.592° SSE |
| 4 mins | 2025-12-06 19:06:24.656Z | 320.401° NNW | 2025-12-06 19:07:24.656Z | 300.795° NW | 20.422° | 2025-12-06 19:10:24.656Z | 246.435° WSW |
| 5 mins | 2025-12-07 05:54:24.656Z | 209.302° SW | 2025-12-07 05:56:24.656Z | 255.621° W | 29.738° | 2025-12-07 05:59:24.656Z | 321.994° 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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