View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55987U 26145.28312307 +.00000000 +00000-0 +42495-4 0 00009
2 55987 43.0049 347.0374 0001672 274.9261 85.1399 15.26746969 01
| Epoch (UTC): | 25 May 2026 06:47:41 |
| Eccentricity: | 0.0001672 |
| inclination: | 43.0049° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 347.0374° |
| argument of perigee: | 274.9261° |
| revolutions per day: | 15.26746969 |
| mean anomaly at epoch: | 85.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|