View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40920U 26053.84937131 +.00000000 +00000-0 +69445-3 0 00001
2 40920 82.4960 150.8557 0009165 232.4865 127.5383 12.42923016 07
| Epoch (UTC): | 22 February 2026 20:23:05 |
| Eccentricity: | 0.0009165 |
| inclination: | 82.4960° |
| perigee height: | 1487 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 150.8557° |
| argument of perigee: | 232.4865° |
| revolutions per day: | 12.42923016 |
| mean anomaly at epoch: | 127.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|