View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60726U 26145.27281765 +.00000000 +00000-0 +27863-4 0 00000
2 60726 53.1591 98.7040 0001012 81.9532 278.1601 15.69700865 09
| Epoch (UTC): | 25 May 2026 06:32:51 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.7040° |
| argument of perigee: | 81.9532° |
| revolutions per day: | 15.69700865 |
| mean anomaly at epoch: | 278.1601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|