View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41654U 00055NT 23150.41034263 .00002796 00000-0 14067-2 0 9998
2 41654 98.6879 203.9759 0046745 140.5916 219.8674 14.16637781366899
| Epoch (UTC): | 30 May 2023 09:50:53 |
| Eccentricity: | 0.0046745 |
| inclination: | 98.6879° |
| perigee height: | 803 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 203.9759° |
| argument of perigee: | 140.5916° |
| revolutions per day: | 14.16637781 |
| mean anomaly at epoch: | 219.8674° |
| orbit number at epoch: | 36689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|