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
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 KUIPER-00388
1 68922U 26098D 26155.10690611 .00017289 00000-0 60986-3 0 9994
2 68922 51.8742 131.8067 0022366 96.6691 263.6839 15.29120491 5329Epoch: 2026-06-04T02:33Z
TLE epoch observation values (Epoch: 2026-06-04T02:33:56.687Z)
Latitude
-0.00002°
Longitude
-159.23544°
Altitude
480.921 km
Speed
7.625 km/s
True Right ascension
08h 47m 13s
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
03:46:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.242 km
Perigee altitude
463.569 km
Semi-major axis
6,857.042 km
Eccentricity
0.00224
Inclination
51.8742°
RAAN
131.8067°
Arg. of periapsis
96.6691°
True anomaly
263.42924°
Mean anomaly
263.6839°
Eccentric anomaly
263.55656°
Mean motion
3.82242 °/min
Orbital period
94.18 mins
BSTAR
0.00060986
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-06 23:44:26.355Z | 194.213° SSW | 2026-06-06 23:47:26.355Z | 125.77° SE | 27.522° | 2026-06-06 23:50:26.355Z | 70.452° E |
| 5 mins | 2026-06-07 01:23:26.355Z | 279.21° WNW | 2026-06-07 01:25:26.355Z | 338.653° N | 29.378° | 2026-06-07 01:28:26.355Z | 37.416° NE |
| 5 mins | 2026-06-07 06:20:26.355Z | 332.711° NNW | 2026-06-07 06:22:26.355Z | 41.739° NE | 33.769° | 2026-06-07 06:25:26.355Z | 103.228° ESE |
| 4 mins | 2026-06-07 07:58:26.355Z | 267.318° W | 2026-06-07 08:00:26.355Z | 219.752° SW | 21.758° | 2026-06-07 08:02:26.355Z | 179.859° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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