KUIPER-00504, 68885
Orbit data source: Space-Track
KUIPER-00504, 68885 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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68885 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00504
1 68885U 26095X 26171.46891397 -.00000178 00000-0 56429-5 0 9999
2 68885 51.9008 241.1417 0000440 94.8625 265.2388 14.79916402 8030Epoch: 2026-06-20T11:15Z
TLE epoch observation values (Epoch: 2026-06-20T11:15:14.167Z)
Latitude
0.00004°
Longitude
163.6496°
Altitude
630.36 km
Speed
7.544 km/s
True Right ascension
16h 04m 34s
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
07:23:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.347 km
Perigee altitude
629.731 km
Semi-major axis
7,008.176 km
Eccentricity
0.00004
Inclination
51.9008°
RAAN
241.1417°
Arg. of periapsis
94.8625°
True anomaly
265.23378°
Mean anomaly
265.2388°
Eccentric anomaly
265.23629°
Mean motion
3.69944 °/min
Orbital period
97.31 mins
BSTAR
0.0000056429
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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-00504 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 06:51:47.219Z | 203.134° SW | 2026-06-21 06:55:47.219Z | 115.799° SE | 34.187° | 2026-06-21 06:58:47.219Z | 67.182° ENE |
| 7 mins | 2026-06-21 08:33:47.219Z | 271.782° WNW | 2026-06-21 08:36:47.219Z | 331.192° NNW | 31.502° | 2026-06-21 08:40:47.219Z | 39.92° NE |
| 4 mins | 2026-06-21 10:17:47.219Z | 328.468° NNW | 2026-06-21 10:19:47.219Z | 1.704° NNE | 17.543° | 2026-06-21 10:21:47.219Z | 30.906° NE |
| 5 mins | 2026-06-21 11:59:47.219Z | 336.381° NNW | 2026-06-21 12:01:47.219Z | 9.523° NNE | 20.907° | 2026-06-21 12:04:47.219Z | 59.345° ENE |
| 7 mins | 2026-06-21 13:40:47.219Z | 314.054° NW | 2026-06-21 13:43:47.219Z | 358.588° N | 41.763° | 2026-06-21 13:47:47.219Z | 116.669° SE |
| 4 mins | 2026-06-21 15:23:47.219Z | 257.789° W | 2026-06-21 15:25:47.219Z | 222.467° SW | 19.14° | 2026-06-21 15:27:47.219Z | 192.241° SSW |
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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