View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64179U 26145.12753797 +.00000000 +00000-0 +97678-3 0 00009
2 64179 53.1598 94.9840 0001388 84.9472 275.1689 15.34401890 01
| Epoch (UTC): | 25 May 2026 03:03:39 |
| Eccentricity: | 0.0001388 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.9840° |
| argument of perigee: | 84.9472° |
| revolutions per day: | 15.34401890 |
| mean anomaly at epoch: | 275.1689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|