View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64802U 26145.46939124 +.00000000 +00000-0 +18479-3 0 00001
2 64802 70.0003 301.0236 0003157 267.9927 92.0870 14.98334130 07
| Epoch (UTC): | 25 May 2026 11:15:55 |
| Eccentricity: | 0.0003157 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.0236° |
| argument of perigee: | 267.9927° |
| revolutions per day: | 14.98334130 |
| mean anomaly at epoch: | 92.0870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|