View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53541U 26145.09179103 +.00000000 +00000-0 +32732-4 0 00000
2 53541 53.2133 91.1343 0001683 55.2000 304.9150 15.08837046 02
| Epoch (UTC): | 25 May 2026 02:12:10 |
| Eccentricity: | 0.0001683 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.1343° |
| argument of perigee: | 55.2000° |
| revolutions per day: | 15.08837046 |
| mean anomaly at epoch: | 304.9150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|