View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00020U 26049.04714715 +.00000000 +00000-0 +35568-3 0 00005
2 00020 33.3445 335.8822 1638126 134.8628 239.7302 11.61829827 07
| Epoch (UTC): | 18 February 2026 01:07:53 |
| Eccentricity: | 0.1638126 |
| inclination: | 33.3445° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 335.8822° |
| argument of perigee: | 134.8628° |
| revolutions per day: | 11.61829827 |
| mean anomaly at epoch: | 239.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|