View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39177U 26145.61301330 +.00000000 +00000-0 +28689-4 0 00002
2 39177 98.0126 113.8916 0012339 86.1684 274.0925 14.56182371 02
| Epoch (UTC): | 25 May 2026 14:42:44 |
| Eccentricity: | 0.0012339 |
| inclination: | 98.0126° |
| perigee height: | 697 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 113.8916° |
| argument of perigee: | 86.1684° |
| revolutions per day: | 14.56182371 |
| mean anomaly at epoch: | 274.0925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|