KUIPER-00282, 69267
Orbit data source: Space-Track
KUIPER-00282, 69267 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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69267 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-00282
1 69267U 26118A 26171.34884485 .00016548 00000-0 50074-3 0 9992
2 69267 51.8599 38.3474 0011822 192.8240 167.2446 15.34257112 4463Epoch: 2026-06-20T08:22Z
TLE epoch observation values (Epoch: 2026-06-20T08:22:20.195Z)
Latitude
-0.00001°
Longitude
4.19849°
Altitude
471.777 km
Speed
7.627 km/s
True Right ascension
02h 33m 23s
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
07:13:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.685 km
Perigee altitude
455.508 km
Semi-major axis
6,841.733 km
Eccentricity
0.00118
Inclination
51.8599°
RAAN
38.3474°
Arg. of periapsis
192.824°
True anomaly
167.27447°
Mean anomaly
167.2446°
Eccentric anomaly
167.25954°
Mean motion
3.83525 °/min
Orbital period
93.87 mins
BSTAR
0.00050074
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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-00282 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 | 2026-06-21 00:31:03.413Z | 314.65° NW | 2026-06-21 00:33:03.413Z | 95.342° ESE | 42.686° | 2026-06-21 00:36:03.413Z | 123.687° SE |
| 5 mins | 2026-06-21 17:23:03.413Z | 206.317° SW | 2026-06-21 17:25:03.413Z | 151.327° SSE | 37.448° | 2026-06-21 17:28:03.413Z | 64.677° ENE |
| 4 mins | 2026-06-21 19:02:03.413Z | 304.294° NW | 2026-06-21 19:03:03.413Z | 330.979° NNW | 23.77° | 2026-06-21 19:06:03.413Z | 31.76° 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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