View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00743U 26088.14333845 +.00000000 +00000-0 +21167-3 0 00002
2 00743 81.5207 230.7166 0174822 193.1765 339.9715 13.26873636 02
| Epoch (UTC): | 29 March 2026 03:26:24 |
| Eccentricity: | 0.0174822 |
| inclination: | 81.5207° |
| perigee height: | 1027 km |
| apogee height: | 1290 km |
| right ascension of ascending node: | 230.7166° |
| argument of perigee: | 193.1765° |
| revolutions per day: | 13.26873636 |
| mean anomaly at epoch: | 339.9715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|