View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56071U 26145.36180723 +.00000000 +00000-0 -14971-3 0 00006
2 56071 87.8989 263.7726 0001640 96.9501 263.1816 13.15548724 01
| Epoch (UTC): | 25 May 2026 08:41:00 |
| Eccentricity: | 0.0001640 |
| inclination: | 87.8989° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7726° |
| argument of perigee: | 96.9501° |
| revolutions per day: | 13.15548724 |
| mean anomaly at epoch: | 263.1816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|