View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20827U 26041.25258632 +.00000000 +00000-0 +18295-4 0 00007
2 20827 82.5301 303.6001 0102880 330.9099 28.6352 13.84643984 01
| Epoch (UTC): | 10 February 2026 06:03:43 |
| Eccentricity: | 0.0102880 |
| inclination: | 82.5301° |
| perigee height: | 872 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 303.6001° |
| argument of perigee: | 330.9099° |
| revolutions per day: | 13.84643984 |
| mean anomaly at epoch: | 28.6352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|