View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53423U 26145.38346344 +.00000000 +00000-0 +17488-4 0 00005
2 53423 53.2147 129.8350 0001238 83.0978 277.0155 15.08842875 03
| Epoch (UTC): | 25 May 2026 09:12:11 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.8350° |
| argument of perigee: | 83.0978° |
| revolutions per day: | 15.08842875 |
| mean anomaly at epoch: | 277.0155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|