View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39460U 26145.38873061 +.00000000 +00000-0 +00000-0 0 00009
2 39460 0.0201 306.0405 0002681 123.5378 48.3497 1.00271604 07
| Epoch (UTC): | 25 May 2026 09:19:46 |
| Eccentricity: | 0.0002681 |
| inclination: | 0.0201° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 306.0405° |
| argument of perigee: | 123.5378° |
| revolutions per day: | 1.00271604 |
| mean anomaly at epoch: | 48.3497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|