View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20826U 26041.24630257 +.00000000 +00000-0 +43057-5 0 00007
2 20826 82.5254 298.7867 0014037 26.7022 333.4858 13.84451684 05
| Epoch (UTC): | 10 February 2026 05:54:40 |
| Eccentricity: | 0.0014037 |
| inclination: | 82.5254° |
| perigee height: | 938 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 298.7867° |
| argument of perigee: | 26.7022° |
| revolutions per day: | 13.84451684 |
| mean anomaly at epoch: | 333.4858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|