View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52271U 26145.32960757 +.00000000 +00000-0 +40577-4 0 00004
2 52271 53.2137 125.0702 0001289 78.2109 281.9028 15.08841781 07
| Epoch (UTC): | 25 May 2026 07:54:38 |
| Eccentricity: | 0.0001289 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.0702° |
| argument of perigee: | 78.2109° |
| revolutions per day: | 15.08841781 |
| mean anomaly at epoch: | 281.9028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|