KUIPER-00293, 68593
Orbit data source: Space-Track
KUIPER-00293, 68593 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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68593 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00293
1 68593U 26072W 26145.58335648 -.00034907 00000-0 -27793-2 0 9993
2 68593 51.8880 288.9177 0013119 317.7227 54.5589 14.99779942 1300Epoch: 2026-05-25T14:00Z
TLE epoch observation values (Epoch: 2026-05-25T14:00:01.999Z)
Latitude
9.71374°
Longitude
-156.58517°
Altitude
562.313 km
Speed
7.585 km/s
True Right ascension
19h 46m 22s
True Declination
9° 39' 18"
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
09:14:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.145 km
Perigee altitude
558.92 km
Semi-major axis
6,946.17 km
Eccentricity
0.00131
Inclination
51.888°
RAAN
288.9177°
Arg. of periapsis
317.7227°
True anomaly
54.68149°
Mean anomaly
54.5589°
Eccentric anomaly
54.62019°
Mean motion
3.74908 °/min
Orbital period
96.02 mins
BSTAR
-0.0027793
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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-00293 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 | 2026-05-26 10:53:50.370Z | 152.55° SSE | 2026-05-26 10:55:50.370Z | 120.061° SE | 14.896° | 2026-05-26 10:57:50.370Z | 91.408° ESE |
| 7 mins | 2026-05-26 12:31:50.370Z | 237.558° WSW | 2026-05-26 12:34:50.370Z | 290.055° WNW | 44.105° | 2026-05-26 12:38:50.370Z | 49.776° ENE |
| 5 mins | 2026-05-26 14:13:50.370Z | 307.87° NW | 2026-05-26 14:15:50.370Z | 346.428° N | 20.616° | 2026-05-26 14:18:50.370Z | 33.146° NE |
| 6 mins | 2026-05-26 17:35:50.370Z | 335.934° NNW | 2026-05-26 17:37:50.370Z | 16.822° NNE | 26.619° | 2026-05-26 17:41:50.370Z | 86.962° E |
| 6 mins | 2026-05-26 19:15:50.370Z | 293.962° NW | 2026-05-26 19:18:50.370Z | 196.153° SSW | 38.84° | 2026-05-26 19:21:50.370Z | 146.767° 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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