KUIPER-00572, 69272
Orbit data source: Space-Track
KUIPER-00572, 69272 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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69272 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-00572
1 69272U 26118F 26170.99634201 .00012636 00000-0 35284-3 0 9997
2 69272 51.8674 39.7554 0007061 181.2910 178.8059 15.37065158 4416Epoch: 2026-06-19T23:54Z
TLE epoch observation values (Epoch: 2026-06-19T23:54:43.949Z)
Latitude
-0.00006°
Longitude
132.85492°
Altitude
460.379 km
Speed
7.635 km/s
True Right ascension
02h 39m 01s
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
07:14:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.086 km
Perigee altitude
450.436 km
Semi-major axis
6,833.398 km
Eccentricity
0.00071
Inclination
51.8674°
RAAN
39.7554°
Arg. of periapsis
181.291°
True anomaly
178.80758°
Mean anomaly
178.8059°
Eccentric anomaly
178.80674°
Mean motion
3.84227 °/min
Orbital period
93.69 mins
BSTAR
0.00035284
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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-00572 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 23:47:29.313Z | 331.983° NNW | 2026-06-20 23:49:29.313Z | 23.684° NE | 29.625° | 2026-06-20 23:52:29.313Z | 94.259° ESE |
| 4 mins | 2026-06-21 01:25:29.313Z | 271.157° WNW | 2026-06-21 01:27:29.313Z | 213.961° SW | 25.893° | 2026-06-21 01:29:29.313Z | 170.96° S |
| 5 mins | 2026-06-21 18:15:29.313Z | 255.131° W | 2026-06-21 18:17:29.313Z | 299.192° NW | 36.171° | 2026-06-21 18:20:29.313Z | 39.182° 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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