View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56077U 26145.31902786 +.00000000 +00000-0 +44108-3 0 00002
2 56077 87.8990 263.7546 0002104 96.7785 263.3585 13.15548018 08
| Epoch (UTC): | 25 May 2026 07:39:24 |
| Eccentricity: | 0.0002104 |
| inclination: | 87.8990° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7546° |
| argument of perigee: | 96.7785° |
| revolutions per day: | 13.15548018 |
| mean anomaly at epoch: | 263.3585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|