View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48315U 26145.25641130 +.00000000 +00000-0 +95472-4 0 00005
2 48315 53.1609 102.8170 0001739 80.8343 279.2855 15.31699730 04
| Epoch (UTC): | 25 May 2026 06:09:13 |
| Eccentricity: | 0.0001739 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 102.8170° |
| argument of perigee: | 80.8343° |
| revolutions per day: | 15.31699730 |
| mean anomaly at epoch: | 279.2855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|