View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20528U 26110.52950300 +.00000000 +00000-0 +51814-4 0 00007
2 20528 82.9394 197.2086 0032822 51.9638 319.4661 13.73149701 02
| Epoch (UTC): | 20 April 2026 12:42:29 |
| Eccentricity: | 0.0032822 |
| inclination: | 82.9394° |
| perigee height: | 964 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 197.2086° |
| argument of perigee: | 51.9638° |
| revolutions per day: | 13.73149701 |
| mean anomaly at epoch: | 319.4661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|