View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62492U 26145.48218189 +.00000000 +00000-0 +46114-3 0 00004
2 62492 42.9990 215.4836 0001019 275.1022 84.9713 15.27595895 05
| Epoch (UTC): | 25 May 2026 11:34:20 |
| Eccentricity: | 0.0001019 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.4836° |
| argument of perigee: | 275.1022° |
| revolutions per day: | 15.27595895 |
| mean anomaly at epoch: | 84.9713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|