View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53167U 26145.34432642 +.00000000 +00000-0 -11801-4 0 00007
2 53167 53.2115 164.9966 0001187 75.0672 285.0452 15.08838708 00
| Epoch (UTC): | 25 May 2026 08:15:49 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.9966° |
| argument of perigee: | 75.0672° |
| revolutions per day: | 15.08838708 |
| mean anomaly at epoch: | 285.0452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|