View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29047U 26106.67218134 +.00000000 +00000-0 +98212-4 0 00008
2 29047 71.9761 77.4580 0048940 342.1306 17.8108 14.31344860 09
| Epoch (UTC): | 16 April 2026 16:07:56 |
| Eccentricity: | 0.0048940 |
| inclination: | 71.9761° |
| perigee height: | 752 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 77.4580° |
| argument of perigee: | 342.1306° |
| revolutions per day: | 14.31344860 |
| mean anomaly at epoch: | 17.8108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|