View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00058U 60013A 23029.87761150 .00000124 00000-0 62393-4 0 9998
2 00058 28.3268 282.3949 0164854 67.6949 294.0985 13.46343725 67592
| Epoch (UTC): | 29 January 2023 21:03:45 |
| Eccentricity: | 0.0164854 |
| inclination: | 28.3268° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 282.3949° |
| argument of perigee: | 67.6949° |
| revolutions per day: | 13.46343725 |
| mean anomaly at epoch: | 294.0985° |
| orbit number at epoch: | 6759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|