View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26077U 00006G 25012.66541120 .00000224 00000-0 24826-3 0 9996
2 26077 70.9691 110.6559 0203773 164.2194 309.3232 13.73158484249531
| Epoch (UTC): | 12 January 2025 15:58:11 |
| Eccentricity: | 0.0203773 |
| inclination: | 70.9691° |
| perigee height: | 838 km |
| apogee height: | 1138 km |
| right ascension of ascending node: | 110.6559° |
| argument of perigee: | 164.2194° |
| revolutions per day: | 13.73158484 |
| mean anomaly at epoch: | 309.3232° |
| orbit number at epoch: | 24953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|