View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04579U 26066.25752905 +.00000000 +00000-0 +14453-3 0 00003
2 04579 74.0005 110.7813 0008899 51.4897 308.7067 14.63592947 03
| Epoch (UTC): | 07 March 2026 06:10:50 |
| Eccentricity: | 0.0008899 |
| inclination: | 74.0005° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 110.7813° |
| argument of perigee: | 51.4897° |
| revolutions per day: | 14.63592947 |
| mean anomaly at epoch: | 308.7067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|