Showing default

ERNST, 60528

Orbit data source: Space-Track

ERNST, 60528 is a German payload satellite in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
60528, 2024-149BN
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
FRAUN
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Sail, 0.8 m
Radar Cross Section
0.110 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 ERNST
1 60528U 24149BN  25353.17000766  .00012028  00000-0  37311-3 0  9997
2 60528  97.3982  71.1478 0005943 212.5869 147.5008 15.33536745 74630
Epoch: 2025-12-19T04:04Z
TLE epoch observation values (Epoch: 2025-12-19T04:04:48.661Z)
Latitude
0.00001°
Longitude
-78.06997°
Altitude
471.811 km
Speed
7.628 km/s
True Right ascension
04h 44m 35s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
15:24:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.283 km
Perigee altitude
458.152 km
Semi-major axis
6,840.355 km
Eccentricity
0.00059
Inclination
97.3982°
RAAN
71.1478°
Arg. of periapsis
212.5869°
True anomaly
147.53737°
Mean anomaly
147.5008°
Eccentric anomaly
147.51909°
Mean motion
3.83641 °/min
Orbital period
93.84 mins
BSTAR
0.00037311
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|