KL-ALPHA B, 44786
Orbit data source: Space-Track
KL-ALPHA B, 44786 is a German payload satellite in LEO that was launched on Sun, 17 Nov 2019 UTC via a KUAIZHOU-1A launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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44786 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
IMI/CAS
Mission
Operational Commercial Communications
Bus & Motor
KLA, Unknown motor
Mass
90 kg wet, ~85 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, Unknown HBR
Radar Cross Section
0.900 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 KL-ALPHA B
1 44786U 19077B 26172.55557550 .00000025 00000-0 17421-4 0 9994
2 44786 88.9107 219.6713 0027975 133.9374 226.4095 13.56003190325773Epoch: 2026-06-21T13:20Z
TLE epoch observation values (Epoch: 2026-06-21T13:20:01.723Z)
Latitude
-0.00002°
Longitude
109.90996°
Altitude
1,067.575 km
Speed
7.311 km/s
True Right ascension
14h 38m 41s
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
21:34:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,068.07 km
Perigee altitude
1,026.525 km
Semi-major axis
7,425.434 km
Eccentricity
0.0028
Inclination
88.9107°
RAAN
219.6713°
Arg. of periapsis
133.9374°
True anomaly
226.17787°
Mean anomaly
226.4095°
Eccentric anomaly
226.29363°
Mean motion
3.39204 °/min
Orbital period
106.13 mins
BSTAR
0.000017421
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Other satellites on launch #77 in the year 2019 (2019-11-17 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.KL-ALPHA B 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-22 14:42:57.167Z | 15.528° NNE | 2026-06-22 14:48:57.167Z | 88.607° E | 33.734° | 2026-06-22 14:53:57.167Z | 151.148° SSE |
| 9 mins | 2026-06-22 16:30:57.167Z | 328.919° NNW | 2026-06-22 16:34:57.167Z | 277.873° WNW | 25.92° | 2026-06-22 16:39:57.167Z | 225.526° WSW |
| 10 mins | 2026-06-23 02:38:57.167Z | 136.521° SSE | 2026-06-23 02:43:57.167Z | 71.797° E | 29.787° | 2026-06-23 02:48:57.167Z | 18.488° NNE |
| 10 mins | 2026-06-23 04:24:57.167Z | 218.14° SW | 2026-06-23 04:29:57.167Z | 283.356° WNW | 30.081° | 2026-06-23 04:34:57.167Z | 339.272° N |
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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