View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02766U 26106.20769810 +.00000000 +00000-0 +00000-0 0 00002
2 02766 36.2292 6.0961 4637331 120.2678 359.7552 0.21273952 09
| Epoch (UTC): | 16 April 2026 04:59:05 |
| Eccentricity: | 0.4637331 |
| inclination: | 36.2292° |
| perigee height: | 57187 km |
| apogee height: | 167121 km |
| right ascension of ascending node: | 6.0961° |
| argument of perigee: | 120.2678° |
| revolutions per day: | 0.21273952 |
| mean anomaly at epoch: | 359.7552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|