View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60120U 26145.34260762 +.00000000 +00000-0 -86988-5 0 00005
2 60120 53.1598 203.3052 0001197 73.4947 286.6203 15.69697821 00
| Epoch (UTC): | 25 May 2026 08:13:21 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.3052° |
| argument of perigee: | 73.4947° |
| revolutions per day: | 15.69697821 |
| mean anomaly at epoch: | 286.6203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|