KUIPER-00606, 69289
Orbit data source: Space-Track
KUIPER-00606, 69289 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Fri, 29 May 2026 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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69289 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 KUIPER-00606
1 69289U 26118Y 26171.05077206 .00020247 00000-0 54626-3 0 9997
2 69289 51.8700 39.3740 0004536 165.0419 195.0703 15.37760304 4428Epoch: 2026-06-20T01:13Z
TLE epoch observation values (Epoch: 2026-06-20T01:13:06.705Z)
Latitude
-0.00003°
Longitude
112.82508°
Altitude
456.488 km
Speed
7.638 km/s
True Right ascension
02h 37m 29s
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
07:13:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.3 km
Perigee altitude
450.103 km
Semi-major axis
6,831.338 km
Eccentricity
0.00045
Inclination
51.87°
RAAN
39.374°
Arg. of periapsis
165.0419°
True anomaly
195.05679°
Mean anomaly
195.0703°
Eccentric anomaly
195.06355°
Mean motion
3.84401 °/min
Orbital period
93.65 mins
BSTAR
0.00054626
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Other satellites on launch #118 in the year 2026 (2026-05-29 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.KUIPER-00606 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 | 2026-06-20 23:31:09.752Z | 339.491° N | 2026-06-20 23:33:09.752Z | 30.682° NE | 24.758° | 2026-06-20 23:35:09.752Z | 77.197° E |
| 4 mins | 2026-06-21 01:09:09.752Z | 277.714° WNW | 2026-06-21 01:10:09.752Z | 247.927° W | 32.578° | 2026-06-21 01:13:09.752Z | 156.687° SSE |
| 5 mins | 2026-06-21 17:59:09.752Z | 245.416° WSW | 2026-06-21 18:01:09.752Z | 4.656° NNE | 42.214° | 2026-06-21 18:04:09.752Z | 48.245° ENE |
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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