View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53866U 26145.35769485 +.00000000 +00000-0 +51318-4 0 00008
2 53866 53.2149 280.1518 0001202 89.6601 270.4528 15.08838944 02
| Epoch (UTC): | 25 May 2026 08:35:04 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 280.1518° |
| argument of perigee: | 89.6601° |
| revolutions per day: | 15.08838944 |
| mean anomaly at epoch: | 270.4528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|