KUIPER-00594, 69279
Orbit data source: Space-Track
KUIPER-00594, 69279 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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69279 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00594
1 69279U 26118N 26171.36258841 .00022207 00000-0 57937-3 0 9992
2 69279 51.8726 37.7144 0000824 87.3388 272.7693 15.38741708 4476Epoch: 2026-06-20T08:42Z
TLE epoch observation values (Epoch: 2026-06-20T08:42:07.638Z)
Latitude
-0.00008°
Longitude
-1.39578°
Altitude
450.565 km
Speed
7.643 km/s
True Right ascension
02h 30m 51s
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
07:13:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.859 km
Perigee altitude
449.734 km
Semi-major axis
6,828.433 km
Eccentricity
0.00008
Inclination
51.8726°
RAAN
37.7144°
Arg. of periapsis
87.3388°
True anomaly
272.75987°
Mean anomaly
272.7693°
Eccentric anomaly
272.76458°
Mean motion
3.84646 °/min
Orbital period
93.59 mins
BSTAR
0.00057937
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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-00594 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 23:11:22.794Z | 352.173° N | 2026-06-20 23:12:22.794Z | 15.482° NNE | 20.115° | 2026-06-20 23:15:22.794Z | 74.626° E |
| 5 mins | 2026-06-21 00:48:22.794Z | 298.775° NW | 2026-06-21 00:50:22.794Z | 222.045° SW | 42.896° | 2026-06-21 00:53:22.794Z | 138.38° SSE |
| 4 mins | 2026-06-21 17:38:22.794Z | 219.742° SW | 2026-06-21 17:40:22.794Z | 79.419° E | 41.076° | 2026-06-21 17:42:22.794Z | 56.949° 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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