View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52500U 26145.16308177 +.00000000 +00000-0 -89669-4 0 00009
2 52500 53.2143 55.8154 0001666 89.9224 270.1959 15.08849131 06
| Epoch (UTC): | 25 May 2026 03:54:50 |
| Eccentricity: | 0.0001666 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.8154° |
| argument of perigee: | 89.9224° |
| revolutions per day: | 15.08849131 |
| mean anomaly at epoch: | 270.1959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|