View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28647U 26088.22327603 +.00000000 +00000-0 +47778-3 0 00005
2 28647 56.9968 162.5870 0063859 54.8479 305.8536 15.43431556 06
| Epoch (UTC): | 29 March 2026 05:21:31 |
| Eccentricity: | 0.0063859 |
| inclination: | 56.9968° |
| perigee height: | 392 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 162.5870° |
| argument of perigee: | 54.8479° |
| revolutions per day: | 15.43431556 |
| mean anomaly at epoch: | 305.8536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|