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 Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 KUIPER-00386
1 68921U 26098C 26207.58335648 -.01772084 00000-0 -14638+0 0 9992
2 68921 51.8919 239.4464 0003130 19.1835 170.5211 15.02128436 5809Epoch: 2026-07-26T14:00Z
TLE epoch observation values (Epoch: 2026-07-26T14:00:01.999Z)
Latitude
-7.74766°
Longitude
-88.74906°
Altitude
564.561 km
Speed
7.579 km/s
True Right ascension
04h 22m 09s
True Declination
-7° 42' 02"
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
21:06:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.963 km
Perigee altitude
558.619 km
Semi-major axis
6,938.928 km
Eccentricity
0.00031
Inclination
51.8919°
RAAN
239.4464°
Arg. of periapsis
19.1835°
True anomaly
170.527°
Mean anomaly
170.5211°
Eccentric anomaly
170.52405°
Mean motion
3.75495 °/min
Orbital period
95.87 mins
BSTAR
-0.14638
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-27 08:42:58.090Z | 327.666° NNW | 2026-07-27 08:44:58.090Z | 357.13° N | 15.529° | 2026-07-27 08:47:58.090Z | 43.127° NE |
| 6 mins | 2026-07-27 10:23:58.090Z | 331.651° NNW | 2026-07-27 10:26:58.090Z | 37.16° NE | 27.128° | 2026-07-27 10:29:58.090Z | 86.573° E |
| 7 mins | 2026-07-27 12:03:58.090Z | 294.025° NW | 2026-07-27 12:06:58.090Z | 217.696° SW | 38.214° | 2026-07-27 12:10:58.090Z | 147.08° SSE |
| 6 mins | 2026-07-28 03:42:58.090Z | 178.473° S | 2026-07-28 03:44:58.090Z | 142.046° SSE | 24.043° | 2026-07-28 03:48:58.090Z | 73.863° E |
| 6 mins | 2026-07-28 05:22:58.090Z | 260.806° W | 2026-07-28 05:25:58.090Z | 350.464° N | 36.259° | 2026-07-28 05:28:58.090Z | 41.331° NE |
| 4 mins | 2026-07-28 07:04:58.090Z | 319.053° NNW | 2026-07-28 07:06:58.090Z | 354.217° N | 17.72° | 2026-07-28 07:08:58.090Z | 25.91° NE |
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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