KUIPER-00254, 68585
Orbit data source: Space-Track
KUIPER-00254, 68585 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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68585 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00254
1 68585U 26072N 26101.50002315 .00052783 00000-0 14449-2 0 9994
2 68585 51.8713 139.4632 0007746 130.9107 114.4081 15.36791941 1301Epoch: 2026-04-11T12:00Z
TLE epoch observation values (Epoch: 2026-04-11T12:00:02.000Z)
Latitude
-45.84566°
Longitude
-6.75388°
Altitude
473.227 km
Speed
7.628 km/s
True Right ascension
00h 51m 53s
True Declination
-45° 39' 60"
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
04:00:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.364 km
Perigee altitude
450.776 km
Semi-major axis
6,834.207 km
Eccentricity
0.00077
Inclination
51.8713°
RAAN
139.4632°
Arg. of periapsis
130.9107°
True anomaly
114.4889°
Mean anomaly
114.4081°
Eccentric anomaly
114.4485°
Mean motion
3.84159 °/min
Orbital period
93.71 mins
BSTAR
0.0014449
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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-00254 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 | 2026-04-12 04:16:16.417Z | 166.548° S | 2026-04-12 04:18:16.417Z | 123.999° SE | 18.297° | 2026-04-12 04:20:16.417Z | 87.093° E |
| 5 mins | 2026-04-12 05:53:16.417Z | 259.232° W | 2026-04-12 05:55:16.417Z | 324.079° NNW | 37.23° | 2026-04-12 05:58:16.417Z | 41.313° NE |
| 4 mins | 2026-04-12 10:49:16.417Z | 344.886° N | 2026-04-12 10:51:16.417Z | 43.115° NE | 24.968° | 2026-04-12 10:53:16.417Z | 83.5° E |
| 5 mins | 2026-04-12 12:26:16.417Z | 284.986° WNW | 2026-04-12 12:28:16.417Z | 231.504° WSW | 32.111° | 2026-04-12 12:31:16.417Z | 157.02° SSE |
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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