Showing default

JCSAT 16, 41729

Orbit data source: Space-Track

JCSAT 16, 41729 is a payload satellite owned by Sky Perfect JSAT (JP) in GEO that was launched on Sun, 14 Aug 2016 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
41729, 2016-050A
Orbit
GEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
LS-1300, R-4D
Mass
~4,600 kg wet, ~2,500 kg dry
Launch date (UTC)
2016-08-14 (9 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 13.5 m
Radar Cross Section
26.964 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 JCSAT 16
1 41729U 16050A   25260.89683758 -.00000271  00000-0  00000-0 0  9995
2 41729   0.0163 160.7907 0001172 306.7734 356.3292  1.00272011 33343
Epoch: 2025-09-17T21:31Z
TLE epoch observation values (Epoch: 2025-09-17T21:31:26.766Z)
Latitude
-0.03306°
Longitude
143.9665°
Altitude
35,781.109 km
Speed
3.075 km/s
True Right ascension
06h 55m 34s
True Declination
0° 01' 59"
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
04:17:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,792.544 km
Perigee altitude
35,782.66 km
Semi-major axis
42,165.739 km
Eccentricity
0.00012
Inclination
0.0163°
RAAN
160.7907°
Arg. of periapsis
306.7734°
True anomaly
356.32834°
Mean anomaly
356.3292°
Eccentric anomaly
356.32877°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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...
Other satellites on launch #50 in the year 2016 (2016-08-14 UTC)

Documentation

Showing up to 5 results
|