View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61764U 26145.63389370 +.00000000 +00000-0 +61370-3 0 00004
2 61764 97.2982 21.6033 0006504 4.4936 355.6374 15.51347944 05
| Epoch (UTC): | 25 May 2026 15:12:48 |
| Eccentricity: | 0.0006504 |
| inclination: | 97.2982° |
| perigee height: | 408 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 21.6033° |
| argument of perigee: | 4.4936° |
| revolutions per day: | 15.51347944 |
| mean anomaly at epoch: | 355.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|