View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13648U 26088.14593352 +.00000000 +00000-0 +70733-4 0 00005
2 13648 73.9950 329.1553 0018759 98.5063 261.8216 14.34773907 07
| Epoch (UTC): | 29 March 2026 03:30:08 |
| Eccentricity: | 0.0018759 |
| inclination: | 73.9950° |
| perigee height: | 762 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 329.1553° |
| argument of perigee: | 98.5063° |
| revolutions per day: | 14.34773907 |
| mean anomaly at epoch: | 261.8216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|