View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36111U 26144.11566036 +.00000000 +00000-0 +00000-0 0 00000
2 36111 64.9981 71.7925 0005494 323.9681 185.3764 2.13103527 04
| Epoch (UTC): | 24 May 2026 02:46:33 |
| Eccentricity: | 0.0005494 |
| inclination: | 64.9981° |
| perigee height: | 19116 km |
| apogee height: | 19144 km |
| right ascension of ascending node: | 71.7925° |
| argument of perigee: | 323.9681° |
| revolutions per day: | 2.13103527 |
| mean anomaly at epoch: | 185.3764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|