KUIPER-00193, 68576
Orbit data source: Space-Track
KUIPER-00193, 68576 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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68576 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: 4 hours ago
TLE from 4 hours ago
0 KUIPER-00193
1 68576U 26072D 26138.83335647 .00024884 00000-0 71121-3 0 9999
2 68576 51.8776 318.7483 0003483 246.9478 211.8014 15.35837390 4151Epoch: 2026-05-18T20:00Z
TLE epoch observation values (Epoch: 2026-05-18T20:00:01.999Z)
Latitude
51.1934°
Longitude
-113.79515°
Altitude
466.41 km
Speed
7.638 km/s
True Right ascension
04h 10m 54s
True Declination
51° 01' 05"
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
09:13:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.282 km
Perigee altitude
456.519 km
Semi-major axis
6,837.037 km
Eccentricity
0.00035
Inclination
51.8776°
RAAN
318.7483°
Arg. of periapsis
246.9478°
True anomaly
211.78037°
Mean anomaly
211.8014°
Eccentric anomaly
211.79089°
Mean motion
3.8392 °/min
Orbital period
93.77 mins
BSTAR
0.00071121
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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-00193 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-19 14:28:44.443Z | 214.998° SW | 2026-05-19 14:31:44.443Z | 159.931° S | 38.209° | 2026-05-19 14:34:44.443Z | 63.634° ENE |
| 4 mins | 2026-05-19 16:08:44.443Z | 305.412° NW | 2026-05-19 16:09:44.443Z | 331.384° NNW | 22.764° | 2026-05-19 16:12:44.443Z | 31.388° NE |
| 5 mins | 2026-05-19 21:03:44.443Z | 320.206° NNW | 2026-05-19 21:05:44.443Z | 60.053° ENE | 41.728° | 2026-05-19 21:08:44.443Z | 117.757° SE |
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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