KUIPER-00297, 68596
Orbit data source: Space-Track
KUIPER-00297, 68596 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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68596 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00297
1 68596U 26072Z 26150.16668980 -.01727545 00000-0 -15204+0 0 9993
2 68596 51.8876 267.1792 0008611 336.3622 131.3573 14.99585705 5221Epoch: 2026-05-30T04:00Z
TLE epoch observation values (Epoch: 2026-05-30T04:00:01.998Z)
Latitude
48.66626°
Longitude
76.98661°
Altitude
577.523 km
Speed
7.576 km/s
True Right ascension
01h 38m 43s
True Declination
48° 29' 28"
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
00:42:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.614 km
Perigee altitude
562.651 km
Semi-major axis
6,946.77 km
Eccentricity
0.00086
Inclination
51.8876°
RAAN
267.1792°
Arg. of periapsis
336.3622°
True anomaly
131.43131°
Mean anomaly
131.3573°
Eccentric anomaly
131.39431°
Mean motion
3.7486 °/min
Orbital period
96.04 mins
BSTAR
-0.15204
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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-00297 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-30 16:48:32.784Z | 318.767° NNW | 2026-05-30 16:51:32.784Z | 24.356° NE | 38.976° | 2026-05-30 16:55:32.784Z | 110.207° ESE |
| 5 mins | 2026-05-30 18:29:32.784Z | 269.964° W | 2026-05-30 18:31:32.784Z | 232.53° WSW | 22.442° | 2026-05-30 18:34:32.784Z | 180.307° SSW |
| 6 mins | 2026-05-31 10:08:32.784Z | 210.857° SW | 2026-05-31 10:11:32.784Z | 106.524° ESE | 39.471° | 2026-05-31 10:14:32.784Z | 60.714° ENE |
| 5 mins | 2026-05-31 11:49:32.784Z | 289.41° WNW | 2026-05-31 11:51:32.784Z | 331.114° NNW | 26.323° | 2026-05-31 11:54:32.784Z | 29.986° NE |
| 4 mins | 2026-05-31 13:31:32.784Z | 329.703° NNW | 2026-05-31 13:33:32.784Z | 2.203° NNE | 15.955° | 2026-05-31 13:35:32.784Z | 32.103° NE |
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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