KUIPER-00198, 67770
Orbit data source: Space-Track
KUIPER-00198, 67770 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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67770 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-00198
1 67770U 26030G 26052.58335648 .00058343 00000-0 16771-2 0 9992
2 67770 51.8811 296.7699 0002347 17.3955 148.7946 15.35246119 1307Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
10.80321°
Longitude
106.69495°
Altitude
461.566 km
Speed
7.637 km/s
True Right ascension
07h 12m 49s
True Declination
10° 44' 14"
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
02:07:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.26 km
Perigee altitude
459.05 km
Semi-major axis
6,838.792 km
Eccentricity
0.00023
Inclination
51.8811°
RAAN
296.7699°
Arg. of periapsis
17.3955°
True anomaly
148.80853°
Mean anomaly
148.7946°
Eccentric anomaly
148.80157°
Mean motion
3.83773 °/min
Orbital period
93.81 mins
BSTAR
0.0016771
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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-00198 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 00:40:41.504Z | 335.461° NNW | 2026-02-22 00:42:41.504Z | 22.418° NNE | 25.57° | 2026-02-22 00:45:41.504Z | 86.314° E |
| 5 mins | 2026-02-22 02:18:41.504Z | 282.834° WNW | 2026-02-22 02:20:41.504Z | 218.758° SW | 33.407° | 2026-02-22 02:23:41.504Z | 154.142° SSE |
| 5 mins | 2026-02-22 19:10:41.504Z | 248.558° W | 2026-02-22 19:12:41.504Z | 346.996° N | 41.909° | 2026-02-22 19:15:41.504Z | 46.709° 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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