View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54779U 26145.43267091 +.00000000 +00000-0 +48548-3 0 00007
2 54779 53.2124 44.7110 0001512 98.6115 261.5048 15.08805413 08
| Epoch (UTC): | 25 May 2026 10:23:02 |
| Eccentricity: | 0.0001512 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.7110° |
| argument of perigee: | 98.6115° |
| revolutions per day: | 15.08805413 |
| mean anomaly at epoch: | 261.5048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|