View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39440U 26038.80174382 +.00000000 +00000-0 +64220-3 0 00002
2 39440 97.8775 347.4472 0060865 96.0027 264.8132 14.92594260 03
| Epoch (UTC): | 07 February 2026 19:14:30 |
| Eccentricity: | 0.0060865 |
| inclination: | 97.8775° |
| perigee height: | 547 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 347.4472° |
| argument of perigee: | 96.0027° |
| revolutions per day: | 14.92594260 |
| mean anomaly at epoch: | 264.8132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|