KUIPER-00386, 68921
Orbit data source: Space-Track
KUIPER-00386, 68921 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 30 Apr 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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68921 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 KUIPER-00386
1 68921U 26098C 26155.12912967 .00018008 00000-0 52143-3 0 9992
2 68921 51.8739 130.4864 0003336 125.6593 234.4704 15.35639073 5341Epoch: 2026-06-04T03:05Z
TLE epoch observation values (Epoch: 2026-06-04T03:05:56.803Z)
Latitude
-0.00002°
Longitude
-168.57812°
Altitude
461.111 km
Speed
7.637 km/s
True Right ascension
08h 41m 56s
True Declination
0° 00' 00"
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
03:01:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.77 km
Perigee altitude
457.208 km
Semi-major axis
6,837.626 km
Eccentricity
0.00033
Inclination
51.8739°
RAAN
130.4864°
Arg. of periapsis
125.6593°
True anomaly
234.4393°
Mean anomaly
234.4704°
Eccentric anomaly
234.45485°
Mean motion
3.83871 °/min
Orbital period
93.78 mins
BSTAR
0.00052143
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Other satellites on launch #98 in the year 2026 (2026-04-30 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-00386 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 | 2026-06-06 23:59:33.945Z | 209.695° SW | 2026-06-07 00:02:33.945Z | 120.945° SE | 36.742° | 2026-06-07 00:05:33.945Z | 62.583° ENE |
| 4 mins | 2026-06-07 01:38:33.945Z | 295.258° NW | 2026-06-07 01:40:33.945Z | 347.886° N | 22.999° | 2026-06-07 01:42:33.945Z | 27.353° NE |
| 5 mins | 2026-06-07 06:33:33.945Z | 319.07° NNW | 2026-06-07 06:35:33.945Z | 13.473° NNE | 40.494° | 2026-06-07 06:38:33.945Z | 113.677° SE |
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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