View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 56265U 22151ACH 24276.49091087 .00010860 00000-0 58279-2 0 9992
2 56265 98.8220 278.1478 0041173 306.8729 52.8672 14.12676361 79275
| Epoch (UTC): | 02 October 2024 11:46:54 |
| Eccentricity: | 0.0041173 |
| inclination: | 98.8220° |
| perigee height: | 820 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 278.1478° |
| argument of perigee: | 306.8729° |
| revolutions per day: | 14.12676361 |
| mean anomaly at epoch: | 52.8672° |
| orbit number at epoch: | 7927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|