KUIPER-00177, 67766
Orbit data source: Space-Track
KUIPER-00177, 67766 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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67766 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-00177
1 67766U 26030C 26052.58335648 .00058477 00000-0 16563-2 0 9994
2 67766 51.8834 296.7335 0000523 86.7033 98.0620 15.35709814 2511Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
-3.85281°
Longitude
118.23328°
Altitude
460.207 km
Speed
7.638 km/s
True Right ascension
07h 58m 58s
True Declination
-3° 49' 44"
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
02:08:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.635 km
Perigee altitude
458.92 km
Semi-major axis
6,837.415 km
Eccentricity
0.00005
Inclination
51.8834°
RAAN
296.7335°
Arg. of periapsis
86.7033°
True anomaly
98.06793°
Mean anomaly
98.062°
Eccentric anomaly
98.06497°
Mean motion
3.83889 °/min
Orbital period
93.78 mins
BSTAR
0.0016563
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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-00177 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-22 00:34:37.431Z | 327.196° NNW | 2026-02-22 00:37:37.431Z | 27.602° NE | 24.212° | 2026-02-22 00:40:37.431Z | 85.427° E |
| 5 mins | 2026-02-22 02:13:37.431Z | 283.886° WNW | 2026-02-22 02:15:37.431Z | 207.085° SW | 35.394° | 2026-02-22 02:18:37.431Z | 149.571° SSE |
| 5 mins | 2026-02-22 19:04:37.431Z | 240.627° WSW | 2026-02-22 19:06:37.431Z | 279.867° WNW | 42.786° | 2026-02-22 19:09:37.431Z | 47.503° ENE |
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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