View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41918U 17003B 23152.18192072 .00000286 00000-0 95134-4 0 9999
2 41918 86.4008 193.1110 0002644 87.3945 272.7554 14.34220485333845
| Epoch (UTC): | 01 June 2023 04:21:57 |
| Eccentricity: | 0.0002644 |
| inclination: | 86.4008° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.1110° |
| argument of perigee: | 87.3945° |
| revolutions per day: | 14.34220485 |
| mean anomaly at epoch: | 272.7554° |
| orbit number at epoch: | 33384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|