View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56079U 26145.38399213 +.00000000 +00000-0 +38108-3 0 00009
2 56079 87.8989 263.7711 0001912 95.3623 264.7725 13.15547255 07
| Epoch (UTC): | 25 May 2026 09:12:56 |
| Eccentricity: | 0.0001912 |
| inclination: | 87.8989° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7711° |
| argument of perigee: | 95.3623° |
| revolutions per day: | 13.15547255 |
| mean anomaly at epoch: | 264.7725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|