View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54161U 26144.98419649 +.00000000 +00000-0 -21018-3 0 00003
2 54161 53.2131 31.7248 0001557 98.4833 261.6336 15.08856573 07
| Epoch (UTC): | 24 May 2026 23:37:14 |
| Eccentricity: | 0.0001557 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.7248° |
| argument of perigee: | 98.4833° |
| revolutions per day: | 15.08856573 |
| mean anomaly at epoch: | 261.6336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|