View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26012U 91068X 25117.28142130 .00000111 00000-0 68899-3 0 9998
2 26012 82.7381 193.0072 0034339 294.0695 130.9811 12.46946053162317
| Epoch (UTC): | 27 April 2025 06:45:14 |
| Eccentricity: | 0.0034339 |
| inclination: | 82.7381° |
| perigee height: | 1450 km |
| apogee height: | 1504 km |
| right ascension of ascending node: | 193.0072° |
| argument of perigee: | 294.0695° |
| revolutions per day: | 12.46946053 |
| mean anomaly at epoch: | 130.9811° |
| orbit number at epoch: | 16231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|