Showing default

SKYBEE-A01, 62671

Orbit data source: Space-Track

SKYBEE-A01, 62671 is a payload satellite owned by ConstellR (DE) in SSO that was launched on Tue, 14 Jan 2025 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
62671, 2025-009BQ
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U MP16, Unknown motor
Mass
110 kg wet, 110 kg dry
Launch date (UTC)
2025-01-14 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 SKYBEE-A01
1 62671U 25009BQ  26307.59531237  .00001585  00000-0  73352-4 0  9994
2 62671  97.3884  23.6741 0004799 187.3170 172.7997 15.21562394157533
Epoch: 2026-11-03T14:17Z
TLE epoch observation values (Epoch: 2026-11-03T14:17:14.988Z)
Latitude
-0.00002°
Longitude
126.50593°
Altitude
507.496 km
Speed
7.608 km/s
True Right ascension
01h 34m 41s
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
14:45:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.39 km
Perigee altitude
494.79 km
Semi-major axis
6,876.227 km
Eccentricity
0.00048
Inclination
97.3884°
RAAN
23.6741°
Arg. of periapsis
187.317°
True anomaly
172.80659°
Mean anomaly
172.7997°
Eccentric anomaly
172.80314°
Mean motion
3.80643 °/min
Orbital period
94.58 mins
BSTAR
0.000073352
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
|