View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56721U 26145.25301024 +.00000000 +00000-0 +12866-3 0 00005
2 56721 87.9097 233.3485 0001829 109.4342 250.6987 13.16593705 01
| Epoch (UTC): | 25 May 2026 06:04:20 |
| Eccentricity: | 0.0001829 |
| inclination: | 87.9097° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3485° |
| argument of perigee: | 109.4342° |
| revolutions per day: | 13.16593705 |
| mean anomaly at epoch: | 250.6987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|