View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13553U 26071.68307044 +.00000000 +00000-0 +58829-4 0 00004
2 13553 82.5690 138.6001 0018872 292.9050 185.7518 14.86669734 00
| Epoch (UTC): | 12 March 2026 16:23:37 |
| Eccentricity: | 0.0018872 |
| inclination: | 82.5690° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 138.6001° |
| argument of perigee: | 292.9050° |
| revolutions per day: | 14.86669734 |
| mean anomaly at epoch: | 185.7518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|