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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00294
1 68594U 26072X 26101.50002315 .00051885 00000-0 14486-2 0 9997
2 68594 51.8672 139.4989 0009808 141.8726 86.5915 15.36168623 1466Epoch: 2026-04-11T12:00Z
TLE epoch observation values (Epoch: 2026-04-11T12:00:02.000Z)
Latitude
-36.34772°
Longitude
-25.16545°
Altitude
468.59 km
Speed
7.632 km/s
True Right ascension
23h 38m 14s
True Declination
-36° 10' 36"
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
04:01:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.624 km
Perigee altitude
451.214 km
Semi-major axis
6,836.056 km
Eccentricity
0.00098
Inclination
51.8672°
RAAN
139.4989°
Arg. of periapsis
141.8726°
True anomaly
86.7037°
Mean anomaly
86.5915°
Eccentric anomaly
86.6476°
Mean motion
3.84003 °/min
Orbital period
93.75 mins
BSTAR
0.0014486
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-12 04:20:39.102Z | 177.611° S | 2026-04-12 04:22:39.102Z | 138.914° SSE | 20.137° | 2026-04-12 04:25:39.102Z | 80.714° E |
| 5 mins | 2026-04-12 05:58:39.102Z | 267.621° W | 2026-04-12 06:00:39.102Z | 344.436° N | 34.795° | 2026-04-12 06:03:39.102Z | 41.756° NE |
| 4 mins | 2026-04-12 10:54:39.102Z | 347.862° N | 2026-04-12 10:55:39.102Z | 16.633° NNE | 26.887° | 2026-04-12 10:58:39.102Z | 88.392° E |
| 5 mins | 2026-04-12 12:31:39.102Z | 279.607° WNW | 2026-04-12 12:33:39.102Z | 222.664° SW | 29.765° | 2026-04-12 12:36:39.102Z | 159.203° S |
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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