View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05560U 26159.52002704 +.00000000 +00000-0 +11389-3 0 00007
2 05560 92.7000 181.0644 0017278 131.8972 228.3711 14.50845003 00
| Epoch (UTC): | 08 June 2026 12:28:50 |
| Eccentricity: | 0.0017278 |
| inclination: | 92.7000° |
| perigee height: | 711 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 181.0644° |
| argument of perigee: | 131.8972° |
| revolutions per day: | 14.50845003 |
| mean anomaly at epoch: | 228.3711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|