View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16864U 26064.15480742 +.00000000 +00000-0 +12062-3 0 00001
2 16864 74.0300 320.9958 0031932 356.8851 3.2101 14.42271531 08
| Epoch (UTC): | 05 March 2026 03:42:55 |
| Eccentricity: | 0.0031932 |
| inclination: | 74.0300° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 320.9958° |
| argument of perigee: | 356.8851° |
| revolutions per day: | 14.42271531 |
| mean anomaly at epoch: | 3.2101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|