KUIPER-00478, 68875
Orbit data source: Space-Track
KUIPER-00478, 68875 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 28 Apr 2026 UTC via an ATLAS V 551 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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68875 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00478
1 68875U 26095M 26171.41503067 .00024154 00000-0 64624-3 0 9990
2 68875 51.8772 226.9250 0008279 330.0692 29.9820 15.37885203 8225Epoch: 2026-06-20T09:57Z
TLE epoch observation values (Epoch: 2026-06-20T09:57:38.649Z)
Latitude
-0.0001°
Longitude
168.8839°
Altitude
448.231 km
Speed
7.647 km/s
True Right ascension
15h 07m 41s
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
07:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.486 km
Perigee altitude
447.175 km
Semi-major axis
6,830.967 km
Eccentricity
0.00083
Inclination
51.8772°
RAAN
226.925°
Arg. of periapsis
330.0692°
True anomaly
30.02945°
Mean anomaly
29.982°
Eccentric anomaly
30.00572°
Mean motion
3.84432 °/min
Orbital period
93.64 mins
BSTAR
0.00064624
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Other satellites on launch #95 in the year 2026 (2026-04-28 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-00478 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 | 2026-06-21 06:25:20.029Z | 223.162° SW | 2026-06-21 06:28:20.029Z | 83.913° E | 41.443° | 2026-06-21 06:31:20.029Z | 55.622° ENE |
| 4 mins | 2026-06-21 08:04:20.029Z | 306.291° NW | 2026-06-21 08:05:20.029Z | 328.445° NNW | 19.499° | 2026-06-21 08:08:20.029Z | 28.094° NE |
| 4 mins | 2026-06-21 11:21:20.029Z | 346.62° N | 2026-06-21 11:23:20.029Z | 29.244° NE | 17.602° | 2026-06-21 11:25:20.029Z | 64.522° ENE |
| 6 mins | 2026-06-21 12:58:20.029Z | 309.337° NW | 2026-06-21 13:01:20.029Z | 117.397° SE | 42.131° | 2026-06-21 13:04:20.029Z | 126.898° SE |
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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