View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39500U 26145.38543727 +.00000000 +00000-0 +00000-0 0 00007
2 39500 0.0805 104.7240 0004211 348.4180 7.1259 1.00271902 02
| Epoch (UTC): | 25 May 2026 09:15:01 |
| Eccentricity: | 0.0004211 |
| inclination: | 0.0805° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 104.7240° |
| argument of perigee: | 348.4180° |
| revolutions per day: | 1.00271902 |
| mean anomaly at epoch: | 7.1259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|