View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65902U 26065.24731538 +.00000000 +00000-0 +16333-2 0 00005
2 65902 53.1603 27.5854 0001164 203.0791 157.0157 15.30221011 09
| Epoch (UTC): | 06 March 2026 05:56:08 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.5854° |
| argument of perigee: | 203.0791° |
| revolutions per day: | 15.30221011 |
| mean anomaly at epoch: | 157.0157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|