View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35935U 09051E 24357.73686862 .00001994 00000-0 43631-3 0 9990
2 35935 98.4503 245.0292 0008711 111.3010 248.9120 14.58846911809745
| Epoch (UTC): | 22 December 2024 17:41:05 |
| Eccentricity: | 0.0008711 |
| inclination: | 98.4503° |
| perigee height: | 691 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 245.0292° |
| argument of perigee: | 111.3010° |
| revolutions per day: | 14.58846911 |
| mean anomaly at epoch: | 248.9120° |
| orbit number at epoch: | 80974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|