View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43822U 26050.09413757 +.00000000 +00000-0 +29468-3 0 00003
2 43822 97.4495 102.8567 0008937 48.1008 312.0985 15.13320251 07
| Epoch (UTC): | 19 February 2026 02:15:33 |
| Eccentricity: | 0.0008937 |
| inclination: | 97.4495° |
| perigee height: | 520 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 102.8567° |
| argument of perigee: | 48.1008° |
| revolutions per day: | 15.13320251 |
| mean anomaly at epoch: | 312.0985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|