View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52567U 26145.34340934 +.00000000 +00000-0 -44336-4 0 00001
2 52567 53.2127 135.0088 0001110 82.5585 277.5533 15.08842400 02
| Epoch (UTC): | 25 May 2026 08:14:30 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.0088° |
| argument of perigee: | 82.5585° |
| revolutions per day: | 15.08842400 |
| mean anomaly at epoch: | 277.5533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|