View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53035U 26145.25739988 +.00000000 +00000-0 -10759-3 0 00004
2 53035 53.2130 90.3936 0001713 86.6866 273.4322 15.08849192 04
| Epoch (UTC): | 25 May 2026 06:10:39 |
| Eccentricity: | 0.0001713 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.3936° |
| argument of perigee: | 86.6866° |
| revolutions per day: | 15.08849192 |
| mean anomaly at epoch: | 273.4322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|