View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33986U 93036FV 24357.48093684 .00003936 00000-0 12237-2 0 9991
2 33986 74.0365 241.3943 0041542 44.2060 9.9965 14.40833724829074
| Epoch (UTC): | 22 December 2024 11:32:32 |
| Eccentricity: | 0.0041542 |
| inclination: | 74.0365° |
| perigee height: | 726 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 241.3943° |
| argument of perigee: | 44.2060° |
| revolutions per day: | 14.40833724 |
| mean anomaly at epoch: | 9.9965° |
| orbit number at epoch: | 82907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|