View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20580U 90037B 23091.35862174 .00006430 00000-0 34874-3 0 9997
2 20580 28.4703 58.9614 0002505 267.1636 222.2285 15.12562595609815
| Epoch (UTC): | 01 April 2023 08:36:24 |
| Eccentricity: | 0.0002505 |
| inclination: | 28.4703° |
| perigee height: | 526 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 58.9614° |
| argument of perigee: | 267.1636° |
| revolutions per day: | 15.12562595 |
| mean anomaly at epoch: | 222.2285° |
| orbit number at epoch: | 60981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|