View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35933U 26073.77613597 +.00000000 +00000-0 +24964-3 0 00007
2 35933 98.4025 339.8391 0005655 148.3380 211.8162 14.61546707 09
| Epoch (UTC): | 14 March 2026 18:37:38 |
| Eccentricity: | 0.0005655 |
| inclination: | 98.4025° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 339.8391° |
| argument of perigee: | 148.3380° |
| revolutions per day: | 14.61546707 |
| mean anomaly at epoch: | 211.8162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|