View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13149U 26039.52447860 +.00000000 +00000-0 +13577-3 0 00003
2 13149 74.0390 220.8725 0012761 6.2790 353.8520 14.36666177 03
| Epoch (UTC): | 08 February 2026 12:35:14 |
| Eccentricity: | 0.0012761 |
| inclination: | 74.0390° |
| perigee height: | 760 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 220.8725° |
| argument of perigee: | 6.2790° |
| revolutions per day: | 14.36666177 |
| mean anomaly at epoch: | 353.8520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|