View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62666U 26145.49275406 +.00000000 +00000-0 +38486-3 0 00006
2 62666 97.4023 227.5956 0005155 59.5574 300.6175 15.29110057 03
| Epoch (UTC): | 25 May 2026 11:49:33 |
| Eccentricity: | 0.0005155 |
| inclination: | 97.4023° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 227.5956° |
| argument of perigee: | 59.5574° |
| revolutions per day: | 15.29110057 |
| mean anomaly at epoch: | 300.6175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|