View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64061U 26145.38338877 +.00000000 +00000-0 +49606-4 0 00004
2 64061 44.9837 123.4920 0011501 278.2225 81.7303 13.99130244 09
| Epoch (UTC): | 25 May 2026 09:12:04 |
| Eccentricity: | 0.0011501 |
| inclination: | 44.9837° |
| perigee height: | 888 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 123.4920° |
| argument of perigee: | 278.2225° |
| revolutions per day: | 13.99130244 |
| mean anomaly at epoch: | 81.7303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|