View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40021U 26071.08851584 +.00000000 +00000-0 +96975-3 0 00004
2 40021 98.0638 117.7991 0005905 78.6004 281.5908 15.50132800 00
| Epoch (UTC): | 12 March 2026 02:07:27 |
| Eccentricity: | 0.0005905 |
| inclination: | 98.0638° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 117.7991° |
| argument of perigee: | 78.6004° |
| revolutions per day: | 15.50132800 |
| mean anomaly at epoch: | 281.5908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|