View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52903U 26145.52891845 +.00000000 +00000-0 +00000-0 0 00002
2 52903 0.0188 256.8740 0002455 108.1073 151.5369 1.00271078 02
| Epoch (UTC): | 25 May 2026 12:41:38 |
| Eccentricity: | 0.0002455 |
| inclination: | 0.0188° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 256.8740° |
| argument of perigee: | 108.1073° |
| revolutions per day: | 1.00271078 |
| mean anomaly at epoch: | 151.5369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|