View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28352U 26018.51062883 +.00000000 +00000-0 -12027-3 0 00009
2 28352 71.0055 52.3356 0011397 347.0549 13.0278 14.12162944 02
| Epoch (UTC): | 18 January 2026 12:15:18 |
| Eccentricity: | 0.0011397 |
| inclination: | 71.0055° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 52.3356° |
| argument of perigee: | 347.0549° |
| revolutions per day: | 14.12162944 |
| mean anomaly at epoch: | 13.0278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|