View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64278U 26145.37362719 +.00000000 +00000-0 +36055-3 0 00008
2 64278 53.1577 120.7259 0001341 89.4389 270.6766 15.30209039 09
| Epoch (UTC): | 25 May 2026 08:58:01 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.7259° |
| argument of perigee: | 89.4389° |
| revolutions per day: | 15.30209039 |
| mean anomaly at epoch: | 270.6766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|