View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39270U 26145.02675236 +.00000000 +00000-0 +32809-3 0 00008
2 39270 81.0015 254.2845 0554383 140.4308 223.8766 14.55547465 06
| Epoch (UTC): | 25 May 2026 00:38:31 |
| Eccentricity: | 0.0554383 |
| inclination: | 81.0015° |
| perigee height: | 315 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 254.2845° |
| argument of perigee: | 140.4308° |
| revolutions per day: | 14.55547465 |
| mean anomaly at epoch: | 223.8766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|