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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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, 2.4 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X44
1 62707U 25009DC 26238.10645747 .00003206 00000-0 28833-3 0 9991
2 62707 97.7029 316.1275 0000893 131.3918 228.7380 14.96350987110395Epoch: 2026-08-26T02:33Z
TLE epoch observation values (Epoch: 2026-08-26T02:33:17.925Z)
Latitude
-0.00005°
Longitude
-56.5614°
Altitude
581.642 km
Speed
7.569 km/s
True Right ascension
21h 04m 30s
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
02:58:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.814 km
Perigee altitude
574.572 km
Semi-major axis
6,953.33 km
Eccentricity
0.00009
Inclination
97.7029°
RAAN
316.1275°
Arg. of periapsis
131.3918°
True anomaly
228.73031°
Mean anomaly
228.738°
Eccentric anomaly
228.73415°
Mean motion
3.74329 °/min
Orbital period
96.17 mins
BSTAR
0.00028833
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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 | 2026-08-26 17:34:40.927Z | 38.473° NE | 2026-08-26 17:37:40.927Z | 100.377° ESE | 28.29° | 2026-08-26 17:40:40.927Z | 157.766° S |
| 4 mins | 2026-08-27 04:23:40.927Z | 103.318° ESE | 2026-08-27 04:25:40.927Z | 66.658° ENE | 19.171° | 2026-08-27 04:27:40.927Z | 30.891° NE |
| 5 mins | 2026-08-27 05:58:40.927Z | 217.047° SW | 2026-08-27 06:00:40.927Z | 262.464° W | 26.543° | 2026-08-27 06:03:40.927Z | 320.423° 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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