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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X44
1 62707U 25009DC 26080.51653474 .00003719 00000-0 34119-3 0 9990
2 62707 97.7093 161.0557 0002769 82.6921 277.4615 14.95467676 86838Epoch: 2026-03-21T12:23Z
TLE epoch observation values (Epoch: 2026-03-21T12:23:48.601Z)
Latitude
0.00001°
Longitude
156.06707°
Altitude
583.72 km
Speed
7.569 km/s
True Right ascension
10h 44m 13s
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
03:52:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.859 km
Perigee altitude
576.007 km
Semi-major axis
6,956.07 km
Eccentricity
0.00028
Inclination
97.7093°
RAAN
161.0557°
Arg. of periapsis
82.6921°
True anomaly
277.43004°
Mean anomaly
277.4615°
Eccentric anomaly
277.44577°
Mean motion
3.74108 °/min
Orbital period
96.23 mins
BSTAR
0.00034119
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 04:36:14.771Z | 118.861° SE | 2026-03-22 04:38:14.771Z | 82.298° E | 24.078° | 2026-03-22 04:41:14.771Z | 20.454° NNE |
| 4 mins | 2026-03-22 06:12:14.771Z | 230.471° WSW | 2026-03-22 06:14:14.771Z | 270.136° WNW | 20.435° | 2026-03-22 06:16:14.771Z | 306.226° NW |
| 6 mins | 2026-03-22 17:53:14.771Z | 31.068° NE | 2026-03-22 17:55:14.771Z | 77.543° E | 37.564° | 2026-03-22 17:59:14.771Z | 176.01° S |
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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