View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24277U 96046A 23344.64625601 .00000113 00000-0 62065-4 0 9991
2 24277 98.9174 6.1773 0000209 267.5539 92.5618 14.29809898424452
| Epoch (UTC): | 10 December 2023 15:30:36 |
| Eccentricity: | 0.0000209 |
| inclination: | 98.9174° |
| perigee height: | 792 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 6.1773° |
| argument of perigee: | 267.5539° |
| revolutions per day: | 14.29809898 |
| mean anomaly at epoch: | 92.5618° |
| orbit number at epoch: | 42445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|