View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60347U 26145.54195785 +.00000000 +00000-0 +61545-4 0 00000
2 60347 53.1610 78.5012 0001284 92.4282 267.6865 15.30192529 00
| Epoch (UTC): | 25 May 2026 13:00:25 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.5012° |
| argument of perigee: | 92.4282° |
| revolutions per day: | 15.30192529 |
| mean anomaly at epoch: | 267.6865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|