ICEYE-X42, 62698
Orbit data source: Space-Track
ICEYE-X42, 62698 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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62698 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, 0.6 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X42
1 62698U 25009CT 25285.17182823 .00004896 00000-0 49099-3 0 9992
2 62698 97.7282 3.0185 0001722 87.7308 272.4108 14.91786468 40316Epoch: 2025-10-12T04:07Z
TLE epoch observation values (Epoch: 2025-10-12T04:07:25.959Z)
Latitude
-0°
Longitude
-79.83245°
Altitude
595.357 km
Speed
7.562 km/s
True Right ascension
00h 12m 04s
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
09:01:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.582 km
Perigee altitude
588.183 km
Semi-major axis
6,967.52 km
Eccentricity
0.00017
Inclination
97.7282°
RAAN
3.0185°
Arg. of periapsis
87.7308°
True anomaly
272.39108°
Mean anomaly
272.4108°
Eccentric anomaly
272.40094°
Mean motion
3.73186 °/min
Orbital period
96.47 mins
BSTAR
0.00049099
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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-X42 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 17:43:00.389Z | 28.806° NE | 2025-10-13 17:47:00.389Z | 113.014° SE | 32.798° | 2025-10-13 17:50:00.389Z | 166.614° S |
| 4 mins | 2025-10-14 04:35:00.389Z | 103.556° ESE | 2025-10-14 04:37:00.389Z | 57.766° ENE | 23.475° | 2025-10-14 04:39:00.389Z | 22.047° NNE |
| 5 mins | 2025-10-14 06:10:00.389Z | 225.392° WSW | 2025-10-14 06:12:00.389Z | 264.11° W | 21.751° | 2025-10-14 06:15:00.389Z | 315.408° 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
Authenticating...
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