View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64419U 26145.52293235 +.00000000 +00000-0 +23392-3 0 00008
2 64419 70.0007 240.8269 0003486 266.9045 93.1715 14.98334502 09
| Epoch (UTC): | 25 May 2026 12:33:01 |
| Eccentricity: | 0.0003486 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.8269° |
| argument of perigee: | 266.9045° |
| revolutions per day: | 14.98334502 |
| mean anomaly at epoch: | 93.1715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|