View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64678U 26145.33042627 +.00000000 +00000-0 +44255-3 0 00002
2 64678 53.1564 131.3672 0001168 92.4726 267.6409 15.30204769 07
| Epoch (UTC): | 25 May 2026 07:55:48 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1564° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.3672° |
| argument of perigee: | 92.4726° |
| revolutions per day: | 15.30204769 |
| mean anomaly at epoch: | 267.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|