View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28353U 26073.54831573 +.00000000 +00000-0 -12488-3 0 00005
2 28353 70.9997 222.2957 0004340 2.5711 357.5432 14.14595913 01
| Epoch (UTC): | 14 March 2026 13:09:34 |
| Eccentricity: | 0.0004340 |
| inclination: | 70.9997° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 222.2957° |
| argument of perigee: | 2.5711° |
| revolutions per day: | 14.14595913 |
| mean anomaly at epoch: | 357.5432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|