View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36499U 26145.56024166 +.00000000 +00000-0 +00000-0 0 00002
2 36499 0.0165 342.5599 0002517 93.7505 249.6170 1.00272426 09
| Epoch (UTC): | 25 May 2026 13:26:44 |
| Eccentricity: | 0.0002517 |
| inclination: | 0.0165° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 342.5599° |
| argument of perigee: | 93.7505° |
| revolutions per day: | 1.00272426 |
| mean anomaly at epoch: | 249.6170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|