View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28054U 26145.61782867 +.00000000 +00000-0 +28807-4 0 00004
2 28054 98.9901 169.2958 0006562 202.4431 311.2800 14.14480222 05
| Epoch (UTC): | 25 May 2026 14:49:40 |
| Eccentricity: | 0.0006562 |
| inclination: | 98.9901° |
| perigee height: | 839 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 169.2958° |
| argument of perigee: | 202.4431° |
| revolutions per day: | 14.14480222 |
| mean anomaly at epoch: | 311.2800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|