View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65604U 26145.46823792 +.00000000 +00000-0 +38044-3 0 00005
2 65604 97.4478 213.9587 0001974 122.2233 237.9186 15.05659852 05
| Epoch (UTC): | 25 May 2026 11:14:15 |
| Eccentricity: | 0.0001974 |
| inclination: | 97.4478° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9587° |
| argument of perigee: | 122.2233° |
| revolutions per day: | 15.05659852 |
| mean anomaly at epoch: | 237.9186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|