View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39075U 26145.58198444 +.00000000 +00000-0 +31649-4 0 00005
2 39075 52.0081 268.4088 0000501 133.1608 226.9301 12.62264910 02
| Epoch (UTC): | 25 May 2026 13:58:03 |
| Eccentricity: | 0.0000501 |
| inclination: | 52.0081° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 268.4088° |
| argument of perigee: | 133.1608° |
| revolutions per day: | 12.62264910 |
| mean anomaly at epoch: | 226.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|