View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63724U 26145.31502846 +.00000000 +00000-0 +66435-3 0 00009
2 63724 51.8999 109.1715 0001072 91.4263 268.6822 14.79898051 00
| Epoch (UTC): | 25 May 2026 07:33:38 |
| Eccentricity: | 0.0001072 |
| inclination: | 51.8999° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 109.1715° |
| argument of perigee: | 91.4263° |
| revolutions per day: | 14.79898051 |
| mean anomaly at epoch: | 268.6822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|