KUIPER-00507, 68887
Orbit data source: Space-Track
KUIPER-00507, 68887 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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68887 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-00507
1 68887U 26095Z 26171.41668980 -.00006672 00000-0 -18991-3 0 9992
2 68887 51.8833 226.5638 0002056 33.8156 157.4091 15.33801293 5814Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-8.94559°
Longitude
-5.02146°
Altitude
468.137 km
Speed
7.632 km/s
True Right ascension
03h 34m 28s
True Declination
-8° 53' 26"
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
07:24:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.355 km
Perigee altitude
463.541 km
Semi-major axis
6,843.085 km
Eccentricity
0.00021
Inclination
51.8833°
RAAN
226.5638°
Arg. of periapsis
33.8156°
True anomaly
157.41815°
Mean anomaly
157.4091°
Eccentric anomaly
157.41362°
Mean motion
3.83412 °/min
Orbital period
93.89 mins
BSTAR
-0.00018991
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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-00507 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:39:24.759Z | 188.894° SSW | 2026-06-21 05:42:24.759Z | 124.517° SE | 24.121° | 2026-06-21 05:44:24.759Z | 82.164° E |
| 4 mins | 2026-06-21 07:18:24.759Z | 281.278° WNW | 2026-06-21 07:19:24.759Z | 312.028° NW | 31.099° | 2026-06-21 07:22:24.759Z | 34.348° NE |
| 4 mins | 2026-06-21 12:14:24.759Z | 340.574° N | 2026-06-21 12:16:24.759Z | 49.483° ENE | 29.98° | 2026-06-21 12:18:24.759Z | 92.35° ESE |
| 4 mins | 2026-06-21 13:52:24.759Z | 261.62° W | 2026-06-21 13:53:24.759Z | 234.095° WSW | 25.353° | 2026-06-21 13:56:24.759Z | 168.902° S |
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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