KUIPER-00215, 67779
Orbit data source: Space-Track
KUIPER-00215, 67779 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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67779 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: 6 hours ago
TLE from 6 hours ago
0 KUIPER-00215
1 67779U 26030R 26052.83335647 -.00014511 00000-0 -42562-3 0 9997
2 67779 51.8839 295.6661 0009891 13.1513 48.5213 15.33826085 1306Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
44.01811°
Longitude
-107.16187°
Altitude
464.256 km
Speed
7.642 km/s
True Right ascension
22h 58m 23s
True Declination
43° 50' 20"
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
05:30:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.642 km
Perigee altitude
458.106 km
Semi-major axis
6,843.011 km
Eccentricity
0.00099
Inclination
51.8839°
RAAN
295.6661°
Arg. of periapsis
13.1513°
True anomaly
48.60629°
Mean anomaly
48.5213°
Eccentric anomaly
48.56379°
Mean motion
3.83418 °/min
Orbital period
93.89 mins
BSTAR
-0.00042562
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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-00215 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 02:30:40.069Z | 287.861° WNW | 2026-02-22 02:33:40.069Z | 226.138° WSW | 27.63° | 2026-02-22 02:36:40.069Z | 163.916° S |
| 4 mins | 2026-02-22 17:47:40.069Z | 163.493° S | 2026-02-22 17:49:40.069Z | 119.791° SE | 18.132° | 2026-02-22 17:51:40.069Z | 84.963° E |
| 5 mins | 2026-02-22 19:24:40.069Z | 259.137° W | 2026-02-22 19:26:40.069Z | 323.006° NNW | 37.313° | 2026-02-22 19:29:40.069Z | 41.146° NE |
| 5 mins | 2026-02-23 00:20:40.069Z | 334.653° NNW | 2026-02-23 00:22:40.069Z | 21.706° NNE | 26.389° | 2026-02-23 00:25:40.069Z | 87.264° E |
| 5 mins | 2026-02-23 01:58:40.069Z | 282.737° WNW | 2026-02-23 02:00:40.069Z | 224.604° SW | 32.459° | 2026-02-23 02:03:40.069Z | 156.667° SSE |
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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