View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35234U 99025DQS 24355.04620405 .00008143 00000-0 15523-2 0 9996
2 35234 98.1044 23.8165 0108431 308.6452 50.5082 14.60529989891242
| Epoch (UTC): | 20 December 2024 01:06:32 |
| Eccentricity: | 0.0108431 |
| inclination: | 98.1044° |
| perigee height: | 615 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 23.8165° |
| argument of perigee: | 308.6452° |
| revolutions per day: | 14.60529989 |
| mean anomaly at epoch: | 50.5082° |
| orbit number at epoch: | 89124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|