View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51960U 26145.12448612 +.00000000 +00000-0 +14415-5 0 00000
2 51960 53.1616 41.1834 0001181 87.6411 272.4725 15.31716087 02
| Epoch (UTC): | 25 May 2026 02:59:15 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1616° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 41.1834° |
| argument of perigee: | 87.6411° |
| revolutions per day: | 15.31716087 |
| mean anomaly at epoch: | 272.4725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|