View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04611U 26045.93975672 +.00000000 +00000-0 +21544-3 0 00009
2 04611 99.8702 39.2860 0124779 76.8851 284.6204 14.03642423 07
| Epoch (UTC): | 14 February 2026 22:33:14 |
| Eccentricity: | 0.0124779 |
| inclination: | 99.8702° |
| perigee height: | 791 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 39.2860° |
| argument of perigee: | 76.8851° |
| revolutions per day: | 14.03642423 |
| mean anomaly at epoch: | 284.6204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|