View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64838U 26145.17808749 +.00000000 +00000-0 -84770-3 0 00004
2 64838 51.9008 314.8441 0000598 101.2901 258.8129 14.79941535 08
| Epoch (UTC): | 25 May 2026 04:16:26 |
| Eccentricity: | 0.0000598 |
| inclination: | 51.9008° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 314.8441° |
| argument of perigee: | 101.2901° |
| revolutions per day: | 14.79941535 |
| mean anomaly at epoch: | 258.8129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|