View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57366U 26145.47905890 +.00000000 +00000-0 +17023-4 0 00007
2 57366 43.0030 167.9719 0001240 273.0437 87.0273 15.27575600 07
| Epoch (UTC): | 25 May 2026 11:29:50 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.9719° |
| argument of perigee: | 273.0437° |
| revolutions per day: | 15.27575600 |
| mean anomaly at epoch: | 87.0273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|