View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43822U 26111.10941281 +.00000000 +00000-0 +21453-3 0 00007
2 43822 97.4371 162.4831 0008019 176.8761 183.2523 15.14018166 08
| Epoch (UTC): | 21 April 2026 02:37:33 |
| Eccentricity: | 0.0008019 |
| inclination: | 97.4371° |
| perigee height: | 518 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 162.4831° |
| argument of perigee: | 176.8761° |
| revolutions per day: | 15.14018166 |
| mean anomaly at epoch: | 183.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|