View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48676U 26145.32337605 +.00000000 +00000-0 +29373-4 0 00009
2 48676 53.1601 117.9913 0001046 84.8756 275.2364 15.29365678 00
| Epoch (UTC): | 25 May 2026 07:45:39 |
| Eccentricity: | 0.0001046 |
| inclination: | 53.1601° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 117.9913° |
| argument of perigee: | 84.8756° |
| revolutions per day: | 15.29365678 |
| mean anomaly at epoch: | 275.2364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|