View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43812U 26040.63011137 +.00000000 +00000-0 +21435-3 0 00003
2 43812 97.3748 82.4027 0004698 218.9958 141.0932 15.07831894 06
| Epoch (UTC): | 09 February 2026 15:07:21 |
| Eccentricity: | 0.0004698 |
| inclination: | 97.3748° |
| perigee height: | 540 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 82.4027° |
| argument of perigee: | 218.9958° |
| revolutions per day: | 15.07831894 |
| mean anomaly at epoch: | 141.0932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|