View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62073U 26145.43660972 +.00000000 +00000-0 +41834-3 0 00009
2 62073 53.1591 197.2919 0001295 81.6245 278.4905 15.34397214 09
| Epoch (UTC): | 25 May 2026 10:28:43 |
| Eccentricity: | 0.0001295 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 197.2919° |
| argument of perigee: | 81.6245° |
| revolutions per day: | 15.34397214 |
| mean anomaly at epoch: | 278.4905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|