View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62292U 26145.58739338 +.00000000 +00000-0 +50457-4 0 00003
2 62292 59.9145 339.4207 0016067 344.5220 15.5294 13.75203728 08
| Epoch (UTC): | 25 May 2026 14:05:50 |
| Eccentricity: | 0.0016067 |
| inclination: | 59.9145° |
| perigee height: | 969 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 339.4207° |
| argument of perigee: | 344.5220° |
| revolutions per day: | 13.75203728 |
| mean anomaly at epoch: | 15.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|