View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39206U 26144.90497066 +.00000000 +00000-0 +00000-0 0 00001
2 39206 4.9498 45.4947 0050225 178.6720 156.1395 1.00269215 00
| Epoch (UTC): | 24 May 2026 21:43:09 |
| Eccentricity: | 0.0050225 |
| inclination: | 4.9498° |
| perigee height: | 35576 km |
| apogee height: | 35999 km |
| right ascension of ascending node: | 45.4947° |
| argument of perigee: | 178.6720° |
| revolutions per day: | 1.00269215 |
| mean anomaly at epoch: | 156.1395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|