KUIPER-00160, 67765
Orbit data source: Space-Track
KUIPER-00160, 67765 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 12 Feb 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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67765 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00160
1 67765U 26030B 26052.58335648 .00056292 00000-0 16380-2 0 9993
2 67765 51.8810 296.7939 0004085 16.8205 137.4104 15.34875913 1300Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
20.0216°
Longitude
98.76258°
Altitude
463.68 km
Speed
7.637 km/s
True Right ascension
06h 41m 05s
True Declination
19° 54' 23"
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
02:06:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.548 km
Perigee altitude
458.96 km
Semi-major axis
6,839.891 km
Eccentricity
0.00041
Inclination
51.881°
RAAN
296.7939°
Arg. of periapsis
16.8205°
True anomaly
137.44207°
Mean anomaly
137.4104°
Eccentric anomaly
137.42623°
Mean motion
3.8368 °/min
Orbital period
93.83 mins
BSTAR
0.001638
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Other satellites on launch #30 in the year 2026 (2026-02-12 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-00160 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 | 2026-02-22 00:44:05.949Z | 334.724° NNW | 2026-02-22 00:46:05.949Z | 22.538° NE | 26.525° | 2026-02-22 00:49:05.949Z | 87.979° E |
| 5 mins | 2026-02-22 02:22:05.949Z | 280.868° WNW | 2026-02-22 02:24:05.949Z | 219.858° SW | 31.83° | 2026-02-22 02:27:05.949Z | 156.538° SSE |
| 5 mins | 2026-02-22 19:14:05.949Z | 249.955° W | 2026-02-22 19:16:05.949Z | 316.729° NNW | 41.079° | 2026-02-22 19:19:05.949Z | 44.518° 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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