View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20U 59007A 25074.19518558 .00001399 00000-0 56594-3 0 9997
2 20 33.3401 117.6886 1644525 115.5193 262.4335 11.60495111431278
| Epoch (UTC): | 15 March 2025 04:41:04 |
| Eccentricity: | 0.1644525 |
| inclination: | 33.3401° |
| perigee height: | 507 km |
| apogee height: | 3218 km |
| right ascension of ascending node: | 117.6886° |
| argument of perigee: | 115.5193° |
| revolutions per day: | 11.60495111 |
| mean anomaly at epoch: | 262.4335° |
| orbit number at epoch: | 43127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|