View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28220U 26145.14876837 +.00000000 +00000-0 +40182-3 0 00007
2 28220 97.8692 221.7324 0007125 103.2211 256.9825 15.33070199 08
| Epoch (UTC): | 25 May 2026 03:34:13 |
| Eccentricity: | 0.0007125 |
| inclination: | 97.8692° |
| perigee height: | 462 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 221.7324° |
| argument of perigee: | 103.2211° |
| revolutions per day: | 15.33070199 |
| mean anomaly at epoch: | 256.9825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|