View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13649U 26087.79265198 +.00000000 +00000-0 +99704-4 0 00009
2 13649 74.0000 218.2371 0018562 339.1411 128.4770 14.38632709 06
| Epoch (UTC): | 28 March 2026 19:01:25 |
| Eccentricity: | 0.0018562 |
| inclination: | 74.0000° |
| perigee height: | 750 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 218.2371° |
| argument of perigee: | 339.1411° |
| revolutions per day: | 14.38632709 |
| mean anomaly at epoch: | 128.4770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|