View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54035U 26145.60489375 +.00000000 +00000-0 +32892-3 0 00007
2 54035 97.3804 150.3952 0022645 89.2265 271.1566 15.21918607 04
| Epoch (UTC): | 25 May 2026 14:31:02 |
| Eccentricity: | 0.0022645 |
| inclination: | 97.3804° |
| perigee height: | 484 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 150.3952° |
| argument of perigee: | 89.2265° |
| revolutions per day: | 15.21918607 |
| mean anomaly at epoch: | 271.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|