KUIPER-00317, 68600
Orbit data source: Space-Track
KUIPER-00317, 68600 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Sat, 04 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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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: 6 days ago
TLE from 6 days ago
0 KUIPER-00317
1 68600U 26072AD 26154.50586512 .00031014 00000-0 82368-3 0 9996
2 68600 51.8695 243.2050 0009912 331.8994 28.1456 15.37960191 9276Epoch: 2026-06-03T12:08Z
TLE epoch observation values (Epoch: 2026-06-03T12:08:26.746Z)
Latitude
-0.00008°
Longitude
169.12999°
Altitude
446.937 km
Speed
7.649 km/s
True Right ascension
16h 12m 49s
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
19:27:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.38 km
Perigee altitude
445.839 km
Semi-major axis
6,830.747 km
Eccentricity
0.00099
Inclination
51.8695°
RAAN
243.205°
Arg. of periapsis
331.8994°
True anomaly
28.19924°
Mean anomaly
28.1456°
Eccentric anomaly
28.17241°
Mean motion
3.84451 °/min
Orbital period
93.64 mins
BSTAR
0.00082368
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Other satellites on launch #72 in the year 2026 (2026-04-04 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-00317 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-09 12:04:01.694Z | 354.524° N | 2026-06-09 12:05:01.694Z | 20.459° NNE | 22.445° | 2026-06-09 12:08:01.694Z | 80.381° E |
| 5 mins | 2026-06-09 13:41:01.694Z | 290.068° WNW | 2026-06-09 13:43:01.694Z | 208.266° SW | 38.853° | 2026-06-09 13:46:01.694Z | 145.072° SSE |
| 5 mins | 2026-06-10 06:31:01.694Z | 233.096° WSW | 2026-06-10 06:33:01.694Z | 46.283° ENE | 42.997° | 2026-06-10 06:36:01.694Z | 51.902° ENE |
| 4 mins | 2026-06-10 08:09:01.694Z | 308.251° NW | 2026-06-10 08:11:01.694Z | 351.787° N | 17.468° | 2026-06-10 08:13:01.694Z | 26.526° NE |
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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