View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40014U 26106.95241176 +.00000000 +00000-0 +43700-4 0 00000
2 40014 98.0413 195.9589 0029012 32.6902 327.6116 15.14971687 03
| Epoch (UTC): | 16 April 2026 22:51:28 |
| Eccentricity: | 0.0029012 |
| inclination: | 98.0413° |
| perigee height: | 501 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 195.9589° |
| argument of perigee: | 32.6902° |
| revolutions per day: | 15.14971687 |
| mean anomaly at epoch: | 327.6116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|