View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41465U 16026B 23091.13287448 .00037615 00000-0 58428-3 0 9999
2 41465 97.0107 323.9539 0008288 149.3482 1.6073 15.53829380387983
| Epoch (UTC): | 01 April 2023 03:11:20 |
| Eccentricity: | 0.0008288 |
| inclination: | 97.0107° |
| perigee height: | 400 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 323.9539° |
| argument of perigee: | 149.3482° |
| revolutions per day: | 15.53829380 |
| mean anomaly at epoch: | 1.6073° |
| orbit number at epoch: | 38798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|