KUIPER-00483, 68878
Orbit data source: Space-Track
KUIPER-00483, 68878 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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68878 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00483
1 68878U 26095Q 26171.46123811 .00001254 00000-0 20848-3 0 9999
2 68878 51.8994 237.8577 0002160 151.5376 208.5703 14.76614001 8071Epoch: 2026-06-20T11:04Z
TLE epoch observation values (Epoch: 2026-06-20T11:04:10.972Z)
Latitude
-0.00004°
Longitude
163.13642°
Altitude
642.109 km
Speed
7.537 km/s
True Right ascension
15h 51m 25s
True Declination
0° 00' 00"
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
07:21:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.999 km
Perigee altitude
638.967 km
Semi-major axis
7,018.62 km
Eccentricity
0.00022
Inclination
51.8994°
RAAN
237.8577°
Arg. of periapsis
151.5376°
True anomaly
208.55847°
Mean anomaly
208.5703°
Eccentric anomaly
208.56438°
Mean motion
3.69118 °/min
Orbital period
97.53 mins
BSTAR
0.00020848
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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-00483 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 06:43:01.057Z | 208.698° SW | 2026-06-21 06:47:01.057Z | 138.039° SSE | 37.104° | 2026-06-21 06:51:01.057Z | 63.417° ENE |
| 7 mins | 2026-06-21 08:26:01.057Z | 276.019° WNW | 2026-06-21 08:29:01.057Z | 337.523° N | 30.515° | 2026-06-21 08:33:01.057Z | 40.414° NE |
| 4 mins | 2026-06-21 10:10:01.057Z | 328.339° NNW | 2026-06-21 10:12:01.057Z | 0.972° NNE | 17.722° | 2026-06-21 10:14:01.057Z | 30.531° NE |
| 6 mins | 2026-06-21 11:52:01.057Z | 332.822° NNW | 2026-06-21 11:55:01.057Z | 24.127° NE | 21.774° | 2026-06-21 11:58:01.057Z | 67.801° E |
| 7 mins | 2026-06-21 13:34:01.057Z | 313.427° NW | 2026-06-21 13:37:01.057Z | 43.351° NE | 43.928° | 2026-06-21 13:41:01.057Z | 121.234° SE |
| 4 mins | 2026-06-21 15:17:01.057Z | 252.353° W | 2026-06-21 15:18:01.057Z | 235.899° WSW | 17.813° | 2026-06-21 15:21:01.057Z | 191.94° 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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