KUIPER-00505, 68886
Orbit data source: Space-Track
KUIPER-00505, 68886 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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68886 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-00505
1 68886U 26095Y 26171.41668980 -.00045668 00000-0 -55679-2 0 9992
2 68886 51.8999 231.4095 0001397 88.8994 98.2274 14.83058007 5507Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-5.7242°
Longitude
-2.74697°
Altitude
621.498 km
Speed
7.549 km/s
True Right ascension
03h 43m 34s
True Declination
-5° 41' 22"
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
07:24:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.118 km
Perigee altitude
619.162 km
Semi-major axis
6,998.277 km
Eccentricity
0.00014
Inclination
51.8999°
RAAN
231.4095°
Arg. of periapsis
88.8994°
True anomaly
98.24324°
Mean anomaly
98.2274°
Eccentric anomaly
98.23532°
Mean motion
3.70729 °/min
Orbital period
97.11 mins
BSTAR
-0.0055679
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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-00505 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 06:20:13.689Z | 212.151° SW | 2026-06-21 06:24:13.689Z | 154.064° SSE | 37.641° | 2026-06-21 06:28:13.689Z | 63.292° ENE |
| 6 mins | 2026-06-21 08:03:13.689Z | 278.848° WNW | 2026-06-21 08:06:13.689Z | 341.613° N | 29.058° | 2026-06-21 08:09:13.689Z | 34.297° NE |
| 5 mins | 2026-06-21 09:46:13.689Z | 323.132° NNW | 2026-06-21 09:48:13.689Z | 354.132° N | 17.178° | 2026-06-21 09:51:13.689Z | 37.385° NE |
| 6 mins | 2026-06-21 11:28:13.689Z | 333.247° NNW | 2026-06-21 11:31:13.689Z | 25.567° NE | 21.468° | 2026-06-21 11:34:13.689Z | 69.169° E |
| 7 mins | 2026-06-21 13:09:13.689Z | 311.512° NW | 2026-06-21 13:12:13.689Z | 344.73° N | 42.999° | 2026-06-21 13:16:13.689Z | 121.768° SE |
| 4 mins | 2026-06-21 14:52:13.689Z | 252.508° W | 2026-06-21 14:53:13.689Z | 236.312° WSW | 16.785° | 2026-06-21 14:56:13.689Z | 192.75° 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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