View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00005U 58002B 23335.27774442 .00000666 00000-0 82667-3 0 9993
2 00005 34.2604 300.2997 1843115 271.7817 67.3740 10.85124451342313
| Epoch (UTC): | 01 December 2023 06:39:57 |
| Eccentricity: | 0.1843115 |
| inclination: | 34.2604° |
| perigee height: | 651 km |
| apogee height: | 3828 km |
| right ascension of ascending node: | 300.2997° |
| argument of perigee: | 271.7817° |
| revolutions per day: | 10.85124451 |
| mean anomaly at epoch: | 67.3740° |
| orbit number at epoch: | 34231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|