View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54100U 26145.63087113 +.00000000 +00000-0 -45367-4 0 00000
2 54100 53.2113 348.4285 0001584 85.5521 274.5652 15.08845830 08
| Epoch (UTC): | 25 May 2026 15:08:27 |
| Eccentricity: | 0.0001584 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.4285° |
| argument of perigee: | 85.5521° |
| revolutions per day: | 15.08845830 |
| mean anomaly at epoch: | 274.5652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|