View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39973U 26087.41446002 +.00000000 +00000-0 +13530-2 0 00002
2 39973 83.0291 339.8177 0020455 68.4227 291.9151 14.55019051 08
| Epoch (UTC): | 28 March 2026 09:56:49 |
| Eccentricity: | 0.0020455 |
| inclination: | 83.0291° |
| perigee height: | 695 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 339.8177° |
| argument of perigee: | 68.4227° |
| revolutions per day: | 14.55019051 |
| mean anomaly at epoch: | 291.9151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|