View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52548U 26145.43080925 +.00000000 +00000-0 -17417-4 0 00001
2 52548 53.2123 144.6163 0001260 51.5443 308.5662 15.08838689 04
| Epoch (UTC): | 25 May 2026 10:20:21 |
| Eccentricity: | 0.0001260 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 144.6163° |
| argument of perigee: | 51.5443° |
| revolutions per day: | 15.08838689 |
| mean anomaly at epoch: | 308.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|