KUIPER-00294, 68594
Orbit data source: Space-Track
KUIPER-00294, 68594 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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68594 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: 17 hours ago
TLE from 17 hours ago
0 KUIPER-00294
1 68594U 26072X 26149.91570897 -.00000688 00000-0 -81389-5 0 9995
2 68594 51.8691 265.6818 0012092 324.9259 35.0930 15.36388609 8566Epoch: 2026-05-29T21:58Z
TLE epoch observation values (Epoch: 2026-05-29T21:58:37.255Z)
Latitude
-0.00004°
Longitude
48.58731°
Altitude
450.802 km
Speed
7.647 km/s
True Right ascension
17h 42m 43s
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
00:45:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.532 km
Perigee altitude
449.001 km
Semi-major axis
6,835.403 km
Eccentricity
0.00121
Inclination
51.8691°
RAAN
265.6818°
Arg. of periapsis
324.9259°
True anomaly
35.17276°
Mean anomaly
35.093°
Eccentric anomaly
35.13287°
Mean motion
3.84058 °/min
Orbital period
93.74 mins
BSTAR
-0.0000081389
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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-00294 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 | 2026-05-30 15:35:21.213Z | 339.211° N | 2026-05-30 15:37:21.213Z | 19.449° NNE | 19.297° | 2026-05-30 15:39:21.213Z | 60.86° ENE |
| 5 mins | 2026-05-30 17:13:21.213Z | 304.85° NW | 2026-05-30 17:15:21.213Z | 237.817° WSW | 44.735° | 2026-05-30 17:18:21.213Z | 132.043° SE |
| 5 mins | 2026-05-31 10:04:21.213Z | 215.988° SW | 2026-05-31 10:06:21.213Z | 156.621° SSE | 41.713° | 2026-05-31 10:09:21.213Z | 59.441° ENE |
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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