View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51963U 26145.65535645 +.00000000 +00000-0 +21553-4 0 00004
2 51963 53.1615 15.5899 0001267 88.2110 271.9036 15.31703616 01
| Epoch (UTC): | 25 May 2026 15:43:42 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 15.5899° |
| argument of perigee: | 88.2110° |
| revolutions per day: | 15.31703616 |
| mean anomaly at epoch: | 271.9036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|