KL-ALPHA A, 44785
Orbit data source: Space-Track
KL-ALPHA A, 44785 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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44785 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
70 kg wet, ~65 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: 4 hours ago
TLE from 4 hours ago
0 KL-ALPHA A
1 44785U 19077A 26095.29118258 .00000181 00000-0 24059-3 0 9993
2 44785 88.9214 230.5369 0009915 330.6334 29.4261 13.56035071315853Epoch: 2026-04-05T06:59Z
TLE epoch observation values (Epoch: 2026-04-05T06:59:18.174Z)
Latitude
-0.00011°
Longitude
-67.88754°
Altitude
1,046.682 km
Speed
7.332 km/s
True Right ascension
15h 22m 08s
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
16:42:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,054.543 km
Perigee altitude
1,039.819 km
Semi-major axis
7,425.318 km
Eccentricity
0.00099
Inclination
88.9214°
RAAN
230.5369°
Arg. of periapsis
330.6334°
True anomaly
29.48198°
Mean anomaly
29.4261°
Eccentric anomaly
29.45403°
Mean motion
3.39212 °/min
Orbital period
106.13 mins
BSTAR
0.00024059
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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 A 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 | 2026-04-05 20:00:08.189Z | 36.134° NE | 2026-04-05 20:04:08.189Z | 80.105° E | 21.359° | 2026-04-05 20:08:08.189Z | 123.121° SE |
| 10 mins | 2026-04-05 21:46:08.189Z | 345.981° N | 2026-04-05 21:50:08.189Z | 290.717° WNW | 39.066° | 2026-04-05 21:56:08.189Z | 202.803° SW |
| 7 mins | 2026-04-06 07:56:08.189Z | 107.689° ESE | 2026-04-06 07:59:08.189Z | 76.751° E | 17.935° | 2026-04-06 08:03:08.189Z | 35.972° NE |
| 11 mins | 2026-04-06 09:40:08.189Z | 192.169° SSW | 2026-04-06 09:45:08.189Z | 286.229° WNW | 42.406° | 2026-04-06 09:51:08.189Z | 353.399° 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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