View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27432U 02024C 23152.85456824 .00000063 00000-0 56161-4 0 9993
2 27432 99.0235 187.2700 0050501 11.0708 161.6015 14.14214276 86209
| Epoch (UTC): | 01 June 2023 20:30:34 |
| Eccentricity: | 0.0050501 |
| inclination: | 99.0235° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 187.2700° |
| argument of perigee: | 11.0708° |
| revolutions per day: | 14.14214276 |
| mean anomaly at epoch: | 161.6015° |
| orbit number at epoch: | 8620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|