KL-ALPHA B
NORAD 44786
Payload
LEO
2019-077B
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LEO · NORAD 44786
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
1030 km
Apogee
1071 km
Inclination
88.9°
Period
106.2 min
Mean Motion
13.56003215 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,051 km
Orbital Velocity26,383 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.56
Eccentricity0.0028
Semi-Major Axis7,422 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇩🇪 KLEO Connect (Germany)
Launch Date
2019-11-17
Launch Site
Jiuquan, China
Int'l Designator
2019-077B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
KL-ALPHA B is an active satellite operated by KLEO Connect (Germany), launched on 2019-11-17 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 1,030 km and 1,071 km with an inclination of 88.9°. It travels at approximately 26,383 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks KL-ALPHA B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
KL-ALPHA B orbits at an average altitude of 1,051 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of KL-ALPHA B’s average altitude, there are currently 180 active payloads and 468 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 88.9°, KL-ALPHA B passes over latitudes between 88.9°N and 88.9°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Germany operates approximately 80 active satellites in total, of which 2 share a similar altitude band with KL-ALPHA B.
❓ Frequently Asked Questions
KL-ALPHA B orbits in Low Earth Orbit (LEO) at altitudes between 1,030 km (perigee) and 1,071 km (apogee), with an average altitude of approximately 1,051 km. It completes one orbit every 106 minutes, travelling at approximately 26,383 km/h (16,394 mph).
KL-ALPHA B is operated by KLEO Connect (Germany). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 44786. You can track KL-ALPHA B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KL-ALPHA B was launched on 2019-11-17 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks KL-ALPHA B (NORAD ID 44786) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
KL-ALPHA B travels at approximately 26,383 km/h (16,394 mph) — roughly 7.33 km/s. It completes 13.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.