View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64030U 26145.43160466 +.00000000 +00000-0 +27728-3 0 00003
2 64030 70.0013 281.1094 0003138 265.9713 94.1087 14.98335952 07
| Epoch (UTC): | 25 May 2026 10:21:30 |
| Eccentricity: | 0.0003138 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1094° |
| argument of perigee: | 265.9713° |
| revolutions per day: | 14.98335952 |
| mean anomaly at epoch: | 94.1087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|