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 Air Force Eastern Test Range (AFETR). 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 KUIPER-00408
1 68924U 26098F 26126.25002315 .00057802 00000-0 17859-2 0 9993
2 68924 51.8773 269.8420 0014722 3.6506 43.5651 15.32871456 2041Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
35.45904°
Longitude
-10.51327°
Altitude
462.484 km
Speed
7.644 km/s
True Right ascension
20h 14m 25s
True Declination
35° 17' 23"
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
20:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.794 km
Perigee altitude
457.637 km
Semi-major axis
6,845.853 km
Eccentricity
0.00147
Inclination
51.8773°
RAAN
269.842°
Arg. of periapsis
3.6506°
True anomaly
43.68152°
Mean anomaly
43.5651°
Eccentric anomaly
43.62329°
Mean motion
3.83179 °/min
Orbital period
93.95 mins
BSTAR
0.0017859
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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 | 2026-05-06 13:52:08.446Z | 284.049° WNW | 2026-05-06 13:54:08.446Z | 324.046° NNW | 22.755° | 2026-05-06 13:57:08.446Z | 28.975° NE |
| 5 mins | 2026-05-06 18:49:08.446Z | 322.207° NNW | 2026-05-06 18:51:08.446Z | 72.765° E | 40.736° | 2026-05-06 18:54:08.446Z | 117.742° SE |
| 5 mins | 2026-05-07 11:42:08.446Z | 198.89° SSW | 2026-05-07 11:44:08.446Z | 144.692° SSE | 33.545° | 2026-05-07 11:47:08.446Z | 67.918° E |
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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