View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53294U 26145.41007519 +.00000000 +00000-0 +14097-3 0 00005
2 53294 53.2143 189.5456 0001243 85.2614 274.8520 15.08852809 01
| Epoch (UTC): | 25 May 2026 09:50:30 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.5456° |
| argument of perigee: | 85.2614° |
| revolutions per day: | 15.08852809 |
| mean anomaly at epoch: | 274.8520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|