View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48776U 26145.56144808 +.00000000 +00000-0 +36953-3 0 00008
2 48776 87.9006 263.6865 0001821 97.0701 263.0636 13.15547197 05
| Epoch (UTC): | 25 May 2026 13:28:29 |
| Eccentricity: | 0.0001821 |
| inclination: | 87.9006° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6865° |
| argument of perigee: | 97.0701° |
| revolutions per day: | 13.15547197 |
| mean anomaly at epoch: | 263.0636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|