View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47762U 26145.49449620 +.00000000 +00000-0 +64966-3 0 00009
2 47762 53.1579 206.4076 0005884 347.4678 12.6193 15.69315980 06
| Epoch (UTC): | 25 May 2026 11:52:04 |
| Eccentricity: | 0.0005884 |
| inclination: | 53.1579° |
| perigee height: | 357 km |
| apogee height: | 365 km |
| right ascension of ascending node: | 206.4076° |
| argument of perigee: | 347.4678° |
| revolutions per day: | 15.69315980 |
| mean anomaly at epoch: | 12.6193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|