KUIPER-00482, 68877
Orbit data source: Space-Track
KUIPER-00482, 68877 is an American payload satellite in LEO that was launched on Tue, 28 Apr 2026 UTC launched 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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68877 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 KUIPER-00482
1 68877U 26095P 26122.16670139 .00001810 00000-0 57927-4 0 9998
2 68877 51.8827 104.8774 0002833 95.5269 118.9860 15.38062424 1371Epoch: 2026-05-02T04:00Z
TLE epoch observation values (Epoch: 2026-05-02T04:00:03.000Z)
Latitude
-26.69055°
Longitude
27.87155°
Altitude
460.529 km
Speed
7.636 km/s
True Right ascension
20h 31m 53s
True Declination
-26° 32' 48"
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
18:39:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.24 km
Perigee altitude
450.37 km
Semi-major axis
6,830.442 km
Eccentricity
0.00028
Inclination
51.8827°
RAAN
104.8774°
Arg. of periapsis
95.5269°
True anomaly
119.01439°
Mean anomaly
118.986°
Eccentric anomaly
119.0002°
Mean motion
3.84477 °/min
Orbital period
93.63 mins
BSTAR
0.000057927
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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-00482 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-03 01:04:09.327Z | 203.825° SW | 2026-05-03 01:07:09.327Z | 130.85° SE | 32.556° | 2026-05-03 01:10:09.327Z | 66.835° ENE |
| 4 mins | 2026-05-03 02:43:09.327Z | 292.038° WNW | 2026-05-03 02:44:09.327Z | 317.68° NNW | 24.844° | 2026-05-03 02:47:09.327Z | 29.693° NE |
| 5 mins | 2026-05-03 07:38:09.327Z | 329.381° NNW | 2026-05-03 07:40:09.327Z | 52.092° ENE | 36.556° | 2026-05-03 07:43:09.327Z | 109.461° ESE |
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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