NSL-1, 44391 (Decayed)
Orbit data source: Space-Track
NSL-1, 44391 was an Israeli payload satellite in LEO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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44391 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 year ago
Origin
NSLComm (BeetleSat) (Unknown / ISRA)Manufacturer
AAC ClydeSpace
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Dish, 0.5 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & history
TLE from 1 year ago
0 NSL-1
1 44391U 19038E 24218.25224336 .15623426 28611-5 15061-2 0 9993
2 44391 97.8531 233.2807 0011701 237.5528 122.4638 16.38276424279796Epoch: 2024-08-05T06:03Z
TLE epoch observation values (Epoch: 2024-08-05T06:03:13.826Z)
Latitude
-0.00004°
Longitude
-171.81364°
Altitude
177.747 km
Speed
7.797 km/s
True Right ascension
15h 33m 07s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
174.881 km
Perigee altitude
159.564 km
Semi-major axis
6,545.359 km
Eccentricity
0.00117
Inclination
97.8531°
RAAN
233.2807°
Arg. of periapsis
237.5528°
True anomaly
122.57684°
Mean anomaly
122.4638°
Eccentric anomaly
122.52033°
Mean motion
4.09867 °/min
Orbital period
87.83 mins
BSTAR
0.0015061
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Other satellites on launch #38 in the year 2019 (2019-07-05 UTC)
NSL-1 Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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