KUIPER-00567, 69626
Orbit data source: Space-Track
KUIPER-00567, 69626 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 17 Jun 2026 UTC via an ARIANE 64 launch vehicle from the French Guiana (FRGUI). 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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69626 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00567
1 69626U 26140AL 26178.50002315 .00025466 00000-0 67484-3 0 9997
2 69626 51.8781 348.7431 0013434 201.0668 81.2772 15.38096117 2795Epoch: 2026-06-27T12:00Z
TLE epoch observation values (Epoch: 2026-06-27T12:00:02.000Z)
Latitude
-50.34407°
Longitude
-177.17309°
Altitude
467.605 km
Speed
7.633 km/s
True Right ascension
18h 33m 47s
True Declination
-50° 10' 04"
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
09:21:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.382 km
Perigee altitude
443.03 km
Semi-major axis
6,830.343 km
Eccentricity
0.00134
Inclination
51.8781°
RAAN
348.7431°
Arg. of periapsis
201.0668°
True anomaly
81.4294°
Mean anomaly
81.2772°
Eccentric anomaly
81.3533°
Mean motion
3.84485 °/min
Orbital period
93.63 mins
BSTAR
0.00067484
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Other satellites on launch #140 in the year 2026 (2026-06-17 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-00567 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 | 2026-06-28 13:27:44.238Z | 191.117° SSW | 2026-06-28 13:29:44.238Z | 138.485° SSE | 29.829° | 2026-06-28 13:32:44.238Z | 70.731° E |
| 4 mins | 2026-06-28 15:05:44.238Z | 285.762° WNW | 2026-06-28 15:07:44.238Z | 346.195° N | 27.108° | 2026-06-28 15:09:44.238Z | 29.33° NE |
| 5 mins | 2026-06-28 20:00:44.238Z | 330.423° NNW | 2026-06-28 20:02:44.238Z | 39.567° NE | 34.689° | 2026-06-28 20:05:44.238Z | 104.779° ESE |
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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