View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 51881C 22022AF 24358.19076389 .00004703 00000+0 29484-3 0 3588
2 51881 53.2148 181.0871 0001317 90.1820 125.9952 15.08839594 12
| Epoch (UTC): | 23 December 2024 04:34:42 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 181.0871° |
| argument of perigee: | 90.1820° |
| revolutions per day: | 15.08839594 |
| mean anomaly at epoch: | 125.9952° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|