ICEYE-X81, 69889
Orbit data source: Space-Track
ICEYE-X81, 69889 is a payload satellite owned by ICEYE (US) in SSO that was launched on Tue, 07 Jul 2026 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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69889 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE
Mission
Operational spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX + PAN, 0.8 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X81
1 69889U 26156W 26211.21982526 .00002238 00000-0 22918-3 0 9997
2 69889 97.7541 111.2927 0007158 73.0339 287.1664 14.91482551 3416Epoch: 2026-07-30T05:16Z
TLE epoch observation values (Epoch: 2026-07-30T05:16:32.902Z)
Latitude
0.00001°
Longitude
84.29213°
Altitude
594.884 km
Speed
7.563 km/s
True Right ascension
07h 25m 10s
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
14:10:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.319 km
Perigee altitude
585.343 km
Semi-major axis
6,968.468 km
Eccentricity
0.00072
Inclination
97.7541°
RAAN
111.2927°
Arg. of periapsis
73.0339°
True anomaly
287.08801°
Mean anomaly
287.1664°
Eccentric anomaly
287.12721°
Mean motion
3.7311 °/min
Orbital period
96.49 mins
BSTAR
0.00022918
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Other satellites on launch #156 in the year 2026 (2026-07-07 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-X81 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 | 2026-07-31 06:00:04.703Z | 24.774° NE | 2026-07-31 06:03:04.703Z | 89.585° E | 39.476° | 2026-07-31 06:07:04.703Z | 178.492° S |
| 5 mins | 2026-07-31 16:51:04.703Z | 122.123° SE | 2026-07-31 16:53:04.703Z | 75.151° E | 29.505° | 2026-07-31 16:56:04.703Z | 12.344° NNE |
| 4 mins | 2026-07-31 18:27:04.703Z | 236.12° WSW | 2026-07-31 18:29:04.703Z | 270.609° WNW | 16.849° | 2026-07-31 18:31:04.703Z | 302.806° NW |
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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