KUIPER-00388, 68922
Orbit data source: Space-Track
KUIPER-00388, 68922 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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68922 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 shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 KUIPER-00388
1 68922U 26098D 26170.93430849 .00017945 00000-0 66486-3 0 9997
2 68922 51.8772 56.3521 0021719 153.4167 206.7935 15.27493468 7747Epoch: 2026-06-19T22:25Z
TLE epoch observation values (Epoch: 2026-06-19T22:25:24.253Z)
Latitude
0.00005°
Longitude
171.84492°
Altitude
497.377 km
Speed
7.61 km/s
True Right ascension
03h 45m 24s
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
07:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.676 km
Perigee altitude
468.869 km
Semi-major axis
6,861.91 km
Eccentricity
0.00217
Inclination
51.8772°
RAAN
56.3521°
Arg. of periapsis
153.4167°
True anomaly
206.68158°
Mean anomaly
206.7935°
Eccentric anomaly
206.73751°
Mean motion
3.81835 °/min
Orbital period
94.28 mins
BSTAR
0.00066486
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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-00388 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 | 2026-06-20 20:39:38.267Z | 285.111° WNW | 2026-06-20 20:42:38.267Z | 342.985° N | 21.386° | 2026-06-20 20:44:38.267Z | 23.058° NE |
| 4 mins | 2026-06-20 23:59:38.267Z | 350.238° N | 2026-06-21 00:00:38.267Z | 10.704° NNE | 18.09° | 2026-06-21 00:03:38.267Z | 66.235° ENE |
| 5 mins | 2026-06-21 01:37:38.267Z | 310.646° NW | 2026-06-21 01:39:38.267Z | 35.372° NE | 44.824° | 2026-06-21 01:42:38.267Z | 125.857° SE |
| 5 mins | 2026-06-21 18:34:38.267Z | 214.508° SW | 2026-06-21 18:36:38.267Z | 163.637° S | 40.977° | 2026-06-21 18:39:38.267Z | 60.859° ENE |
| 4 mins | 2026-06-21 20:13:38.267Z | 297.307° NW | 2026-06-21 20:15:38.267Z | 344.327° N | 22.207° | 2026-06-21 20:17:38.267Z | 24.309° 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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