View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39059U 26104.23400230 +.00000000 +00000-0 +31816-3 0 00008
2 39059 82.4978 261.6571 0026715 171.4314 188.7227 12.42937575 06
| Epoch (UTC): | 14 April 2026 05:36:57 |
| Eccentricity: | 0.0026715 |
| inclination: | 82.4978° |
| perigee height: | 1473 km |
| apogee height: | 1515 km |
| right ascension of ascending node: | 261.6571° |
| argument of perigee: | 171.4314° |
| revolutions per day: | 12.42937575 |
| mean anomaly at epoch: | 188.7227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|