View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13777U 26107.73229773 +.00000000 +00000-0 +63225-4 0 00006
2 13777 99.0514 289.9238 0020366 132.3636 227.9257 14.00896460 09
| Epoch (UTC): | 17 April 2026 17:34:30 |
| Eccentricity: | 0.0020366 |
| inclination: | 99.0514° |
| perigee height: | 876 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 289.9238° |
| argument of perigee: | 132.3636° |
| revolutions per day: | 14.00896460 |
| mean anomaly at epoch: | 227.9257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|