KUIPER-00178, 67767
Orbit data source: Space-Track
KUIPER-00178, 67767 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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67767 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-00178
1 67767U 26030D 26052.58335648 .00055929 00000-0 16346-2 0 9993
2 67767 51.8832 296.8055 0005301 3.6273 146.1317 15.34734960 1890Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
23.38159°
Longitude
95.57856°
Altitude
465.374 km
Speed
7.635 km/s
True Right ascension
06h 28m 21s
True Declination
23° 15' 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
02:10:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.799 km
Perigee altitude
458.547 km
Semi-major axis
6,840.31 km
Eccentricity
0.00053
Inclination
51.8832°
RAAN
296.8055°
Arg. of periapsis
3.6273°
True anomaly
146.16553°
Mean anomaly
146.1317°
Eccentric anomaly
146.14862°
Mean motion
3.83645 °/min
Orbital period
93.84 mins
BSTAR
0.0016346
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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-00178 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-22 00:46:16.779Z | 350.275° N | 2026-02-22 00:47:16.779Z | 19.324° NNE | 26.783° | 2026-02-22 00:50:16.779Z | 87.734° E |
| 5 mins | 2026-02-22 02:23:16.779Z | 281.453° WNW | 2026-02-22 02:25:16.779Z | 224.418° SW | 31.338° | 2026-02-22 02:28:16.779Z | 158.058° S |
| 5 mins | 2026-02-22 19:15:16.779Z | 249.786° W | 2026-02-22 19:17:16.779Z | 300.613° NW | 39.911° | 2026-02-22 19:20:16.779Z | 43.145° 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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