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: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X44
1 62707U 25009DC 26192.76507090 .00002183 00000-0 19893-3 0 9999
2 62707 97.7055 271.5025 0002641 79.6019 280.5499 14.96153599103614Epoch: 2026-07-11T18:21Z
TLE epoch observation values (Epoch: 2026-07-11T18:21:42.125Z)
Latitude
-0.00013°
Longitude
66.4034°
Altitude
581.508 km
Speed
7.57 km/s
True Right ascension
18h 06m 00s
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
17:10:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.642 km
Perigee altitude
573.969 km
Semi-major axis
6,953.942 km
Eccentricity
0.00026
Inclination
97.7055°
RAAN
271.5025°
Arg. of periapsis
79.6019°
True anomaly
280.52015°
Mean anomaly
280.5499°
Eccentric anomaly
280.53502°
Mean motion
3.7428 °/min
Orbital period
96.18 mins
BSTAR
0.00019893
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-12 05:43:02.329Z | 190.519° SSW | 2026-07-12 05:46:02.329Z | 246.012° WSW | 34.516° | 2026-07-12 05:50:02.329Z | 333.295° NNW |
| 5 mins | 2026-07-12 17:26:02.329Z | 60.048° ENE | 2026-07-12 17:28:02.329Z | 104.349° ESE | 22.744° | 2026-07-12 17:31:02.329Z | 151.843° SSE |
| 5 mins | 2026-07-12 19:01:02.329Z | 328.246° NNW | 2026-07-12 19:03:02.329Z | 287.06° WNW | 22.018° | 2026-07-12 19:06:02.329Z | 238.149° WSW |
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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