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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X44
1 62707U 25009DC 25286.26187460 .00005197 00000-0 49370-3 0 9993
2 62707 97.7281 4.3532 0001001 171.1873 188.9365 14.93915027 63049Epoch: 2025-10-13T06:17Z
TLE epoch observation values (Epoch: 2025-10-13T06:17:05.965Z)
Latitude
0°
Longitude
-111.98884°
Altitude
589.477 km
Speed
7.565 km/s
True Right ascension
00h 17m 24s
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
08:52:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.454 km
Perigee altitude
582.06 km
Semi-major axis
6,960.894 km
Eccentricity
0.0001
Inclination
97.7281°
RAAN
4.3532°
Arg. of periapsis
171.1873°
True anomaly
188.93472°
Mean anomaly
188.9365°
Eccentric anomaly
188.93561°
Mean motion
3.73719 °/min
Orbital period
96.33 mins
BSTAR
0.0004937
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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 | 2025-10-13 18:05:48.762Z | 15.623° NNE | 2025-10-13 18:09:48.762Z | 122.616° SE | 44.138° | 2025-10-13 18:12:48.762Z | 187.094° SSW |
| 6 mins | 2025-10-14 04:55:48.762Z | 138.185° SSE | 2025-10-14 04:58:48.762Z | 59.793° ENE | 34.675° | 2025-10-14 05:01:48.762Z | 3.968° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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