Showing default

LEMUR 2 DEMBITZ, 42842

Orbit data source: Space-Track

LEMUR 2 DEMBITZ, 42842 is a payload satellite owned by Spire (US) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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.

Loading next visibility...
Identifier
42842, 2017-042T
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2017-07-14 (8 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.093 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 LEMUR 2 DEMBITZ
1 42842U 17042T   25339.24486739  .00028582  00000-0  12185-2 0  9993
2 42842  97.3753 158.0679 0007755 351.8909   8.2202 15.22873184458755
Epoch: 2025-12-05T05:52Z
TLE epoch observation values (Epoch: 2025-12-05T05:52:36.542Z)
Latitude
0.00006°
Longitude
-4.3741°
Altitude
494.996 km
Speed
7.62 km/s
True Right ascension
10h 32m 16s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
18:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.469 km
Perigee altitude
488.811 km
Semi-major axis
6,872.277 km
Eccentricity
0.00078
Inclination
97.3753°
RAAN
158.0679°
Arg. of periapsis
351.8909°
True anomaly
8.23292°
Mean anomaly
8.2202°
Eccentric anomaly
8.22656°
Mean motion
3.80971 °/min
Orbital period
94.5 mins
BSTAR
0.0012185
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|