View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51738U 26145.54213032 +.00000000 +00000-0 -20312-4 0 00008
2 51738 53.2134 334.1147 0001274 86.2144 273.8994 15.08834404 05
| Epoch (UTC): | 25 May 2026 13:00:40 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.1147° |
| argument of perigee: | 86.2144° |
| revolutions per day: | 15.08834404 |
| mean anomaly at epoch: | 273.8994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|