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 23150.48728057 .00000171 00000-0 16781-3 0 9995
2 15752 82.9477 143.3802 0023413 202.7450 157.2670 13.73189477903867
| Epoch (UTC): | 30 May 2023 11:41:41 |
| Eccentricity: | 0.0023413 |
| inclination: | 82.9477° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 143.3802° |
| argument of perigee: | 202.7450° |
| revolutions per day: | 13.73189477 |
| mean anomaly at epoch: | 157.2670° |
| orbit number at epoch: | 90386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|