Name of Satellite, Alternate Names |
Intelsat 26 (JCSat R, JCSAT-4, Japan Communications Satellite 4) |
Country of Operator/Owner |
USA |
Operator/Owner |
Intelsat, Ltd. |
Users |
Commercial |
Purpose |
Communications |
Class of Orbit |
GEO |
Type of Orbit |
|
Longitude of GEO (degrees) |
50 |
Perigee (km) |
35779 |
Apogee (km) |
35794 |
Eccentricity |
0.000177908507584833 |
Inclination (degrees) |
0.02 |
Period (minutes) |
1436.1 |
Launch Mass (kg.) |
3124 |
Dry Mass (kg.) |
1841 |
Power (watts) |
5200 |
Date of Launch |
16-02-1997 |
Expected Lifetime |
12 yrs. |
Contractor |
Boeing Satellite Systems |
Country of Contractor |
USA |
Launch Site |
Cape Canaveral |
Launch Vehicle |
Atlas 2AS |
COSPAR Number |
1997-007A |
NORAD Number |
24732 |
Comments |
Backup for JCSAT-3; 12 C-band, 12 Ku-band; relay voice, data, television signals via Ku-band to eastern Asia, Australia, New Zealand, India; via C-band to eastern and southern Asia and Hawaii. Digital TV. Sold to Intelsat in 2010. |