View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05918U 26138.49972630 +.00000000 +00000-0 +96182-5 0 00007
2 05918 81.2389 54.2169 0057802 171.4902 188.7262 14.06309741 08
| Epoch (UTC): | 18 May 2026 11:59:36 |
| Eccentricity: | 0.0057802 |
| inclination: | 81.2389° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 54.2169° |
| argument of perigee: | 171.4902° |
| revolutions per day: | 14.06309741 |
| mean anomaly at epoch: | 188.7262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|