View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27433U 02024D 23152.07524199 .00000438 00000-0 25886-3 0 9994
2 27433 99.0511 178.4579 0015364 50.8981 309.3554 14.13012397 84177
| Epoch (UTC): | 01 June 2023 01:48:20 |
| Eccentricity: | 0.0015364 |
| inclination: | 99.0511° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 178.4579° |
| argument of perigee: | 50.8981° |
| revolutions per day: | 14.13012397 |
| mean anomaly at epoch: | 309.3554° |
| orbit number at epoch: | 8417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|