View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49456U 26145.51180852 +.00000000 +00000-0 +63597-4 0 00003
2 49456 53.2151 234.3012 0001031 86.3378 273.7732 15.08840430 06
| Epoch (UTC): | 25 May 2026 12:17:00 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.3012° |
| argument of perigee: | 86.3378° |
| revolutions per day: | 15.08840430 |
| mean anomaly at epoch: | 273.7732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|