KUIPER-00299, 68864
Orbit data source: Space-Track
KUIPER-00299, 68864 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 28 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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68864 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00299
1 68864U 26095A 26171.41668980 -.00020161 00000-0 -28497-2 0 9997
2 68864 51.8982 234.3472 0002363 169.5652 23.2309 14.76443879 4972Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-10.17785°
Longitude
3.75601°
Altitude
641.673 km
Speed
7.539 km/s
True Right ascension
04h 09m 35s
True Declination
-10° 07' 02"
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
07:20:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.681 km
Perigee altitude
639.364 km
Semi-major axis
7,019.159 km
Eccentricity
0.00024
Inclination
51.8982°
RAAN
234.3472°
Arg. of periapsis
169.5652°
True anomaly
23.24158°
Mean anomaly
23.2309°
Eccentric anomaly
23.23624°
Mean motion
3.69076 °/min
Orbital period
97.54 mins
BSTAR
-0.0028497
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Other satellites on launch #95 in the year 2026 (2026-04-28 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-00299 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 06:24:05.538Z | 206.347° SW | 2026-06-21 06:28:05.538Z | 139.904° SSE | 35.463° | 2026-06-21 06:32:05.538Z | 65.067° ENE |
| 7 mins | 2026-06-21 08:07:05.538Z | 273.415° WNW | 2026-06-21 08:10:05.538Z | 335.668° NNW | 31.593° | 2026-06-21 08:14:05.538Z | 40.54° NE |
| 4 mins | 2026-06-21 09:51:05.538Z | 326.911° NNW | 2026-06-21 09:53:05.538Z | 359.652° N | 17.933° | 2026-06-21 09:55:05.538Z | 29.482° NE |
| 6 mins | 2026-06-21 11:33:05.538Z | 331.989° NNW | 2026-06-21 11:36:05.538Z | 22.047° NNE | 21.355° | 2026-06-21 11:39:05.538Z | 65.832° ENE |
| 7 mins | 2026-06-21 13:15:05.538Z | 314.74° NW | 2026-06-21 13:18:05.538Z | 29.264° NE | 43.186° | 2026-06-21 13:22:05.538Z | 118.502° SE |
| 4 mins | 2026-06-21 14:58:05.538Z | 255.367° W | 2026-06-21 14:59:05.538Z | 238.535° WSW | 18.982° | 2026-06-21 15:02:05.538Z | 191.641° SSW |
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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