KUIPER-00364, 68867
Orbit data source: Space-Track
KUIPER-00364, 68867 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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68867 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-00364
1 68867U 26095D 26171.41668980 -.00061458 00000-0 -74099-2 0 9993
2 68867 51.9001 231.3238 0002511 320.4569 90.5355 14.83665850 5359Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
37.83875°
Longitude
-150.03327°
Altitude
620.806 km
Speed
7.553 km/s
True Right ascension
17h 54m 25s
True Declination
37° 40' 08"
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
07:22:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.985 km
Perigee altitude
616.472 km
Semi-major axis
6,996.366 km
Eccentricity
0.00025
Inclination
51.9001°
RAAN
231.3238°
Arg. of periapsis
320.4569°
True anomaly
90.56427°
Mean anomaly
90.5355°
Eccentric anomaly
90.54989°
Mean motion
3.70881 °/min
Orbital period
97.07 mins
BSTAR
-0.0074099
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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-00364 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 05:19:12.168Z | 160.858° S | 2026-06-21 05:21:12.168Z | 132.756° SE | 15.502° | 2026-06-21 05:24:12.168Z | 90.05° ESE |
| 7 mins | 2026-06-21 06:59:12.168Z | 236.095° WSW | 2026-06-21 07:02:12.168Z | 304.294° NW | 44.66° | 2026-06-21 07:06:12.168Z | 50.448° ENE |
| 5 mins | 2026-06-21 08:42:12.168Z | 307.455° NW | 2026-06-21 08:44:12.168Z | 345.753° N | 22.205° | 2026-06-21 08:47:12.168Z | 32.585° NE |
| 4 mins | 2026-06-21 10:25:12.168Z | 342.41° N | 2026-06-21 10:26:12.168Z | 358.659° N | 16.99° | 2026-06-21 10:29:12.168Z | 43.241° NE |
| 6 mins | 2026-06-21 12:06:12.168Z | 332.285° NNW | 2026-06-21 12:09:12.168Z | 35.893° NE | 27.903° | 2026-06-21 12:12:12.168Z | 84.796° E |
| 7 mins | 2026-06-21 13:47:12.168Z | 295.427° NW | 2026-06-21 13:50:12.168Z | 224.011° SW | 39.744° | 2026-06-21 13:54:12.168Z | 146.349° SSE |
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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