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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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: 1 day ago
TLE from 1 day ago
0 ICEYE-X42
1 62698U 25009CT 26170.75568828 .00001746 00000-0 17835-3 0 9997
2 62698 97.7398 249.0245 0001347 91.2636 268.8737 14.91856585 77674Epoch: 2026-06-19T18:08Z
TLE epoch observation values (Epoch: 2026-06-19T18:08:11.467Z)
Latitude
-0.00003°
Longitude
68.99662°
Altitude
595.208 km
Speed
7.562 km/s
True Right ascension
16h 36m 05s
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
07:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.103 km
Perigee altitude
588.226 km
Semi-major axis
6,967.302 km
Eccentricity
0.00013
Inclination
97.7398°
RAAN
249.0245°
Arg. of periapsis
91.2636°
True anomaly
268.85827°
Mean anomaly
268.8737°
Eccentric anomaly
268.86598°
Mean motion
3.73204 °/min
Orbital period
96.46 mins
BSTAR
0.00017835
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:06:06.297Z | 99.483° ESE | 2026-06-21 04:08:06.297Z | 70.365° E | 14.347° | 2026-06-21 04:10:06.297Z | 38.783° NE |
| 6 mins | 2026-06-21 05:41:06.297Z | 197.471° SSW | 2026-06-21 05:43:06.297Z | 240.432° WSW | 34.061° | 2026-06-21 05:47:06.297Z | 332.17° NNW |
| 5 mins | 2026-06-21 17:25:06.297Z | 56.552° ENE | 2026-06-21 17:27:06.297Z | 101.119° ESE | 24.453° | 2026-06-21 17:30:06.297Z | 152.176° SSE |
| 5 mins | 2026-06-21 19:00:06.297Z | 332.747° NNW | 2026-06-21 19:02:06.297Z | 296.586° NW | 21.298° | 2026-06-21 19:05:06.297Z | 243.806° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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