View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04139U 26066.24901662 +.00000000 +00000-0 +16805-3 0 00003
2 04139 74.0298 109.7493 0003645 115.9445 244.2100 14.66471612 00
| Epoch (UTC): | 07 March 2026 05:58:35 |
| Eccentricity: | 0.0003645 |
| inclination: | 74.0298° |
| perigee height: | 670 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 109.7493° |
| argument of perigee: | 115.9445° |
| revolutions per day: | 14.66471612 |
| mean anomaly at epoch: | 244.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|