View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30822U 99025AVG 24356.02972940 .00001126 00000-0 63750-3 0 9997
2 30822 98.7740 27.0445 0074392 216.1163 173.4513 14.10704381916716
| Epoch (UTC): | 21 December 2024 00:42:48 |
| Eccentricity: | 0.0074392 |
| inclination: | 98.7740° |
| perigee height: | 803 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 27.0445° |
| argument of perigee: | 216.1163° |
| revolutions per day: | 14.10704381 |
| mean anomaly at epoch: | 173.4513° |
| orbit number at epoch: | 91671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|