KUIPER-00597, 69282
Orbit data source: Space-Track
KUIPER-00597, 69282 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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69282 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: 20 hours ago
TLE from 20 hours ago
0 KUIPER-00597
1 69282U 26118R 26170.99463764 .00012914 00000-0 36014-3 0 9993
2 69282 51.8650 39.7423 0006949 182.1001 177.9958 15.37083947 4415Epoch: 2026-06-19T23:52Z
TLE epoch observation values (Epoch: 2026-06-19T23:52:16.692Z)
Latitude
0.00004°
Longitude
133.45716°
Altitude
460.245 km
Speed
7.635 km/s
True Right ascension
02h 38m 58s
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
07:11:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.954 km
Perigee altitude
450.457 km
Semi-major axis
6,833.343 km
Eccentricity
0.00069
Inclination
51.865°
RAAN
39.7423°
Arg. of periapsis
182.1001°
True anomaly
177.99858°
Mean anomaly
177.9958°
Eccentric anomaly
177.99719°
Mean motion
3.84232 °/min
Orbital period
93.69 mins
BSTAR
0.00036014
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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-00597 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 23:44:55.108Z | 332.823° NNW | 2026-06-20 23:46:55.108Z | 23.991° NE | 28.835° | 2026-06-20 23:49:55.108Z | 92.93° ESE |
| 4 mins | 2026-06-21 01:22:55.108Z | 272.529° WNW | 2026-06-21 01:24:55.108Z | 213.23° SW | 27.01° | 2026-06-21 01:26:55.108Z | 169.204° S |
| 5 mins | 2026-06-21 18:12:55.108Z | 253.354° W | 2026-06-21 18:14:55.108Z | 297.948° NW | 37.206° | 2026-06-21 18:17:55.108Z | 40.311° NE |
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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