View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60492U 26145.21025559 +.00000000 +00000-0 +39287-3 0 00003
2 60492 97.3772 228.4113 0002258 16.3768 343.7550 15.39018023 06
| Epoch (UTC): | 25 May 2026 05:02:46 |
| Eccentricity: | 0.0002258 |
| inclination: | 97.3772° |
| perigee height: | 447 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 228.4113° |
| argument of perigee: | 16.3768° |
| revolutions per day: | 15.39018023 |
| mean anomaly at epoch: | 343.7550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|