View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13917U 26162.57626846 +.00000000 +00000-0 -23889-5 0 00001
2 13917 82.9423 328.3354 0029695 67.9461 359.1169 13.77128160 03
| Epoch (UTC): | 11 June 2026 13:49:49 |
| Eccentricity: | 0.0029695 |
| inclination: | 82.9423° |
| perigee height: | 952 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 328.3354° |
| argument of perigee: | 67.9461° |
| revolutions per day: | 13.77128160 |
| mean anomaly at epoch: | 359.1169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|