View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 05485U 71080A 23275.73158764 .00000020 00000-0 82850-6 0 9999
2 05485 32.0564 59.9457 0640284 343.7257 14.3622 12.74175253423125
| Epoch (UTC): | 02 October 2023 17:33:29 |
| Eccentricity: | 0.0640284 |
| inclination: | 32.0564° |
| perigee height: | 869 km |
| apogee height: | 1861 km |
| right ascension of ascending node: | 59.9457° |
| argument of perigee: | 343.7257° |
| revolutions per day: | 12.74175253 |
| mean anomaly at epoch: | 14.3622° |
| orbit number at epoch: | 42312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|