View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56061U 26145.56528235 +.00000000 +00000-0 +18543-3 0 00009
2 56061 87.9253 248.4723 0001662 100.9216 259.2105 13.21826334 05
| Epoch (UTC): | 25 May 2026 13:34:00 |
| Eccentricity: | 0.0001662 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4723° |
| argument of perigee: | 100.9216° |
| revolutions per day: | 13.21826334 |
| mean anomaly at epoch: | 259.2105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|