View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 15752U 85041B 23151.50738114 .00000172 00000-0 16933-3 0 9994
2 15752 82.9478 142.6275 0023474 199.8842 160.1400 13.73189823904008
| Epoch (UTC): | 31 May 2023 12:10:37 |
| Eccentricity: | 0.0023474 |
| inclination: | 82.9478° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 142.6275° |
| argument of perigee: | 199.8842° |
| revolutions per day: | 13.73189823 |
| mean anomaly at epoch: | 160.1400° |
| orbit number at epoch: | 90400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|