View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54096U 26145.57200203 +.00000000 +00000-0 +35381-4 0 00008
2 54096 53.2142 348.7708 0001437 90.8224 269.2932 15.08840507 01
| Epoch (UTC): | 25 May 2026 13:43:40 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.7708° |
| argument of perigee: | 90.8224° |
| revolutions per day: | 15.08840507 |
| mean anomaly at epoch: | 269.2932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|