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 23086.16738170 .00029217 00000-0 46070-3 0 9998
2 41465 97.0109 319.1003 0007991 164.5781 312.2461 15.53464238387214
| Epoch (UTC): | 27 March 2023 04:01:01 |
| Eccentricity: | 0.0007991 |
| inclination: | 97.0109° |
| perigee height: | 401 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 319.1003° |
| argument of perigee: | 164.5781° |
| revolutions per day: | 15.53464238 |
| mean anomaly at epoch: | 312.2461° |
| orbit number at epoch: | 38721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|