View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30167U 99025TY 24280.84823083 .00006951 00000-0 17170-2 0 9993
2 30167 99.0123 333.2853 0149327 5.9184 44.7962 14.45857466931110
| Epoch (UTC): | 06 October 2024 20:21:27 |
| Eccentricity: | 0.0149327 |
| inclination: | 99.0123° |
| perigee height: | 633 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 333.2853° |
| argument of perigee: | 5.9184° |
| revolutions per day: | 14.45857466 |
| mean anomaly at epoch: | 44.7962° |
| orbit number at epoch: | 93111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|