View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20775U 26040.14162075 +.00000000 +00000-0 +43401-3 0 00007
2 20775 82.9022 276.9649 0366967 109.6441 254.4767 14.88118565 03
| Epoch (UTC): | 09 February 2026 03:23:56 |
| Eccentricity: | 0.0366967 |
| inclination: | 82.9022° |
| perigee height: | 348 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 276.9649° |
| argument of perigee: | 109.6441° |
| revolutions per day: | 14.88118565 |
| mean anomaly at epoch: | 254.4767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|