View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64047U 26145.34397358 +.00000000 +00000-0 +16519-3 0 00009
2 64047 70.0006 281.2020 0002951 268.2068 91.8753 14.98337903 00
| Epoch (UTC): | 25 May 2026 08:15:19 |
| Eccentricity: | 0.0002951 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.2020° |
| argument of perigee: | 268.2068° |
| revolutions per day: | 14.98337903 |
| mean anomaly at epoch: | 91.8753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|