KUIPER-00408, 68924
Orbit data source: Space-Track
KUIPER-00408, 68924 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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68924 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00408
1 68924U 26098F 26170.91290179 -.00038740 00000-0 -14255-2 0 9991
2 68924 51.8744 56.2312 0015051 164.5410 195.6035 15.27120158 7741Epoch: 2026-06-19T21:54Z
TLE epoch observation values (Epoch: 2026-06-19T21:54:34.714Z)
Latitude
-0.00003°
Longitude
179.45147°
Altitude
495.135 km
Speed
7.613 km/s
True Right ascension
03h 44m 55s
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
08:41:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.221 km
Perigee altitude
474.562 km
Semi-major axis
6,863.028 km
Eccentricity
0.00151
Inclination
51.8744°
RAAN
56.2312°
Arg. of periapsis
164.541°
True anomaly
195.55719°
Mean anomaly
195.6035°
Eccentric anomaly
195.58034°
Mean motion
3.81742 °/min
Orbital period
94.3 mins
BSTAR
-0.0014255
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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-00408 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 | 2026-06-21 01:05:57.069Z | 327.95° NNW | 2026-06-21 01:07:57.069Z | 28.759° NE | 35.746° | 2026-06-21 01:10:57.069Z | 103.852° ESE |
| 5 mins | 2026-06-21 18:03:57.069Z | 182.199° SSW | 2026-06-21 18:05:57.069Z | 128.05° SE | 27.932° | 2026-06-21 18:08:57.069Z | 71.374° E |
| 5 mins | 2026-06-21 19:41:57.069Z | 275.576° WNW | 2026-06-21 19:43:57.069Z | 329.711° NNW | 30.528° | 2026-06-21 19:46:57.069Z | 35.772° 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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