View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40011U 26071.26740330 +.00000000 +00000-0 +19590-3 0 00007
2 40011 97.5454 260.7743 0022331 266.9304 92.9358 14.87853025 01
| Epoch (UTC): | 12 March 2026 06:25:03 |
| Eccentricity: | 0.0022331 |
| inclination: | 97.5454° |
| perigee height: | 589 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 260.7743° |
| argument of perigee: | 266.9304° |
| revolutions per day: | 14.87853025 |
| mean anomaly at epoch: | 92.9358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|