KUIPER-00180, 67768
Orbit data source: Space-Track
KUIPER-00180, 67768 is a payload satellite owned by Kuiper Systems (FR) 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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67768 intel report (Beta)
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Identifier
Orbit
Country
FRRelated 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-00180
1 67768U 26030E 26052.58335648 .00059783 00000-0 18529-2 0 9991
2 67768 51.8807 296.9230 0014720 19.0125 71.1357 15.32756676 1304Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
52.03398°
Longitude
25.91013°
Altitude
470.492 km
Speed
7.639 km/s
True Right ascension
01h 49m 41s
True Declination
51° 51' 36"
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
02:06:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.134 km
Perigee altitude
457.979 km
Semi-major axis
6,846.194 km
Eccentricity
0.00147
Inclination
51.8807°
RAAN
296.923°
Arg. of periapsis
19.0125°
True anomaly
71.29541°
Mean anomaly
71.1357°
Eccentric anomaly
71.21555°
Mean motion
3.8315 °/min
Orbital period
93.96 mins
BSTAR
0.0018529
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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-00180 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 01:02:45.888Z | 333.867° NNW | 2026-02-22 01:04:45.888Z | 37.784° NE | 32.463° | 2026-02-22 01:07:45.888Z | 100.274° ESE |
| 4 mins | 2026-02-22 02:40:45.888Z | 266.764° W | 2026-02-22 02:42:45.888Z | 214.669° SW | 23.578° | 2026-02-22 02:44:45.888Z | 175.333° S |
| 4 mins | 2026-02-22 17:56:45.888Z | 171.699° S | 2026-02-22 17:58:45.888Z | 123.655° SE | 21.628° | 2026-02-22 18:00:45.888Z | 83.878° E |
| 5 mins | 2026-02-22 19:33:45.888Z | 263.124° W | 2026-02-22 19:35:45.888Z | 310.455° NW | 33.026° | 2026-02-22 19:38:45.888Z | 36.29° 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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