KUIPER-00223, 67783
Orbit data source: Space-Track
KUIPER-00223, 67783 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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67783 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: 5 hours ago
TLE from 5 hours ago
0 KUIPER-00223
1 67783U 26030V 26052.83335647 -.00014241 00000-0 -42082-3 0 9999
2 67783 51.8826 295.6823 0011987 12.7455 40.0208 15.33548033 2335Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
38.96713°
Longitude
-116.9459°
Altitude
462.192 km
Speed
7.644 km/s
True Right ascension
22h 19m 15s
True Declination
38° 47' 31"
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
03:51:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.905 km
Perigee altitude
457.498 km
Semi-major axis
6,843.838 km
Eccentricity
0.0012
Inclination
51.8826°
RAAN
295.6823°
Arg. of periapsis
12.7455°
True anomaly
40.10923°
Mean anomaly
40.0208°
Eccentric anomaly
40.06501°
Mean motion
3.83348 °/min
Orbital period
93.91 mins
BSTAR
-0.00042082
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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-00223 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 00:55:35.672Z | 325.027° NNW | 2026-02-22 00:58:35.672Z | 37.331° NE | 30.284° | 2026-02-22 01:01:35.672Z | 97.028° ESE |
| 4 mins | 2026-02-22 02:34:35.672Z | 268.933° W | 2026-02-22 02:36:35.672Z | 211.372° SW | 25.912° | 2026-02-22 02:38:35.672Z | 170.751° S |
| 5 mins | 2026-02-22 19:27:35.672Z | 264.161° W | 2026-02-22 19:29:35.672Z | 338.523° N | 36.073° | 2026-02-22 19:32:35.672Z | 41.689° NE |
| 5 mins | 2026-02-23 00:23:35.672Z | 336.609° NNW | 2026-02-23 00:25:35.672Z | 28.391° NE | 27.294° | 2026-02-23 00:28:35.672Z | 90.266° ESE |
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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