View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26960U 01049D 25197.11911120 .00029374 00000-0 48675-3 0 9995
2 26960 97.6754 268.3471 0022454 120.3866 239.9609 15.51829898300543
| Epoch (UTC): | 16 July 2025 02:51:31 |
| Eccentricity: | 0.0022454 |
| inclination: | 97.6754° |
| perigee height: | 396 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 268.3471° |
| argument of perigee: | 120.3866° |
| revolutions per day: | 15.51829898 |
| mean anomaly at epoch: | 239.9609° |
| orbit number at epoch: | 30054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|