KUIPER-00194, 68577
Orbit data source: Space-Track
KUIPER-00194, 68577 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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68577 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: 8 hours ago
TLE from 8 hours ago
0 KUIPER-00194
1 68577U 26072E 26101.50002315 .00053795 00000-0 14117-2 0 9991
2 68577 51.8761 139.3877 0002990 102.2925 175.9651 15.38113592 1858Epoch: 2026-04-11T12:00Z
TLE epoch observation values (Epoch: 2026-04-11T12:00:02.000Z)
Latitude
-51.28355°
Longitude
42.86381°
Altitude
471.339 km
Speed
7.629 km/s
True Right ascension
04h 10m 21s
True Declination
-51° 06' 31"
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
02:29:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.197 km
Perigee altitude
450.112 km
Semi-major axis
6,830.291 km
Eccentricity
0.0003
Inclination
51.8761°
RAAN
139.3877°
Arg. of periapsis
102.2925°
True anomaly
175.96751°
Mean anomaly
175.9651°
Eccentric anomaly
175.96631°
Mean motion
3.84489 °/min
Orbital period
93.63 mins
BSTAR
0.0014117
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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-00194 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 04:06:23.714Z | 163.729° S | 2026-04-12 04:08:23.714Z | 126.657° SE | 15.157° | 2026-04-12 04:10:23.714Z | 91.582° ESE |
| 5 mins | 2026-04-12 05:43:23.714Z | 251.003° W | 2026-04-12 05:45:23.714Z | 323.619° NNW | 40.813° | 2026-04-12 05:48:23.714Z | 44.604° NE |
| 4 mins | 2026-04-12 10:39:23.714Z | 353.013° N | 2026-04-12 10:40:23.714Z | 19.408° NNE | 23.062° | 2026-04-12 10:43:23.714Z | 81.724° E |
| 5 mins | 2026-04-12 12:16:23.714Z | 287.58° WNW | 2026-04-12 12:18:23.714Z | 212.043° SW | 37.002° | 2026-04-12 12:21:23.714Z | 147.873° 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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