ONEWEB-0700, 61606

Orbit data source: Space-Track

ONEWEB-0700, 61606 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 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
61606, 2024-188N
Orbit
LEO
Country
Flag of UKUK
Related business
Manufacturer
One Web
Mission
Operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
2024-10-20 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 6.7 m
Radar Cross Section
3.464 m², Large (>1 m²)

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

TLE from 5 hours ago
0 ONEWEB-0700
1 61606U 24188N   25336.82568155  .00000008  00000-0 -13690-4 0  9993
2 61606  87.8823  75.2887 0001065  82.2668 277.8581 13.10369229 57587
Epoch: 2025-12-02T19:48Z
TLE epoch observation values (Epoch: 2025-12-02T19:48:58.885Z)
Latitude
0.00003°
Longitude
66.13808°
Altitude
1,224.508 km
Speed
7.242 km/s
True Right ascension
05h 01m 09s
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
22:26:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,219.66 km
Perigee altitude
1,218.042 km
Semi-major axis
7,596.988 km
Eccentricity
0.00011
Inclination
87.8823°
RAAN
75.2887°
Arg. of periapsis
82.2668°
True anomaly
277.84601°
Mean anomaly
277.8581°
Eccentric anomaly
277.85206°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
-0.00001369
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
|