View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65653U 26145.08013400 +.00000000 +00000-0 +32572-3 0 00004
2 65653 97.4473 188.9500 0001298 144.0366 216.0948 15.05654633 04
| Epoch (UTC): | 25 May 2026 01:55:23 |
| Eccentricity: | 0.0001298 |
| inclination: | 97.4473° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.9500° |
| argument of perigee: | 144.0366° |
| revolutions per day: | 15.05654633 |
| mean anomaly at epoch: | 216.0948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|