View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53742U 26145.39077912 +.00000000 +00000-0 -75875-6 0 00009
2 53742 53.2147 279.7242 0001244 98.4509 261.6624 15.08839181 05
| Epoch (UTC): | 25 May 2026 09:22:43 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.7242° |
| argument of perigee: | 98.4509° |
| revolutions per day: | 15.08839181 |
| mean anomaly at epoch: | 261.6624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|