View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65223U 26145.29559936 +.00000000 +00000-0 +34130-3 0 00001
2 65223 53.1598 156.5769 0001196 86.1643 273.9496 15.34398858 09
| Epoch (UTC): | 25 May 2026 07:05:39 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.5769° |
| argument of perigee: | 86.1643° |
| revolutions per day: | 15.34398858 |
| mean anomaly at epoch: | 273.9496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|