View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21048U 26098.22239110 +.00000000 +00000-0 +12420-3 0 00005
2 21048 18.4567 169.4495 1187745 212.9432 139.1073 11.85462217 03
| Epoch (UTC): | 08 April 2026 05:20:14 |
| Eccentricity: | 0.1187745 |
| inclination: | 18.4567° |
| perigee height: | 782 km |
| apogee height: | 2712 km |
| right ascension of ascending node: | 169.4495° |
| argument of perigee: | 212.9432° |
| revolutions per day: | 11.85462217 |
| mean anomaly at epoch: | 139.1073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|