View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53731U 26145.36546421 +.00000000 +00000-0 +15538-2 0 00005
2 53731 53.2143 266.7867 0004334 30.3079 329.8166 15.15327919 05
| Epoch (UTC): | 25 May 2026 08:46:16 |
| Eccentricity: | 0.0004334 |
| inclination: | 53.2143° |
| perigee height: | 517 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 266.7867° |
| argument of perigee: | 30.3079° |
| revolutions per day: | 15.15327919 |
| mean anomaly at epoch: | 329.8166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|