KUIPER-00375, 68868
Orbit data source: Space-Track
KUIPER-00375, 68868 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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68868 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00375
1 68868U 26095E 26171.41668980 -.01123243 00000-0 -47472-1 0 9990
2 68868 51.8885 226.9172 0001959 355.3355 33.3355 15.25836761 4511Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
22.2449°
Longitude
-173.11647°
Altitude
487.685 km
Speed
7.625 km/s
True Right ascension
16h 22m 05s
True Declination
22° 07' 12"
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
10:19:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.081 km
Perigee altitude
487.391 km
Semi-major axis
6,866.873 km
Eccentricity
0.0002
Inclination
51.8885°
RAAN
226.9172°
Arg. of periapsis
355.3355°
True anomaly
33.34784°
Mean anomaly
33.3355°
Eccentric anomaly
33.34167°
Mean motion
3.81421 °/min
Orbital period
94.38 mins
BSTAR
-0.047472
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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-00375 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 06:30:48.056Z | 228.069° WSW | 2026-06-21 06:33:48.056Z | 81.181° E | 44.309° | 2026-06-21 06:36:48.056Z | 53.783° ENE |
| 4 mins | 2026-06-21 08:10:48.056Z | 304.864° NW | 2026-06-21 08:12:48.056Z | 348.384° N | 19.956° | 2026-06-21 08:14:48.056Z | 24.762° NE |
| 4 mins | 2026-06-21 11:29:48.056Z | 343.627° N | 2026-06-21 11:31:48.056Z | 26.503° NE | 20.588° | 2026-06-21 11:33:48.056Z | 65.033° ENE |
| 6 mins | 2026-06-21 13:07:48.056Z | 304.6° NW | 2026-06-21 13:10:48.056Z | 157.66° S | 43.113° | 2026-06-21 13:13:48.056Z | 133.204° 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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