View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54768U 26145.45941251 +.00000000 +00000-0 -25096-4 0 00009
2 54768 53.2126 44.8718 0001589 122.1921 237.9225 15.08835726 09
| Epoch (UTC): | 25 May 2026 11:01:33 |
| Eccentricity: | 0.0001589 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.8718° |
| argument of perigee: | 122.1921° |
| revolutions per day: | 15.08835726 |
| mean anomaly at epoch: | 237.9225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|