Showing default

JCSAT 18, 44868

Orbit data source: Space-Track

JCSAT 18, 44868 is a Japanese payload satellite in GEO that was launched on Tue, 17 Dec 2019 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
44868, 2019-091A
Orbit
GEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Boeing/ES
Mission
Operational Commercial Communications
Bus & Motor
BSS-702MP, R-4D?
Mass
6,800 kg wet, ~3,500 kg dry
Launch date (UTC)
2019-12-17 (7 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, 4.2 m
Radar Cross Section
56.564 m², Large (>1 m²)

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

TLE from 12 hours ago
0 JCSAT 18
1 44868U 19091A   26304.78922159 -.00000205  00000-0  00000-0 0  9996
2 44868   0.0173 258.5366 0000505 328.0361 247.6473  1.00271816 25388
Epoch: 2026-10-31T18:56Z
TLE epoch observation values (Epoch: 2026-10-31T18:56:28.745Z)
Latitude
-0.02096°
Longitude
149.97883°
Altitude
35,786.892 km
Speed
3.075 km/s
True Right ascension
07h 36m 45s
True Declination
0° 01' 15"
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
02:17:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.786 km
Perigee altitude
35,785.527 km
Semi-major axis
42,165.794 km
Eccentricity
0.00005
Inclination
0.0173°
RAAN
258.5366°
Arg. of periapsis
328.0361°
True anomaly
247.64195°
Mean anomaly
247.6473°
Eccentric anomaly
247.64462°
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 #91 in the year 2019 (2019-12-17 UTC)

Documentation

Showing up to 5 results
|