View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62128U 26145.49608108 +.00000000 +00000-0 +98703-3 0 00006
2 62128 43.0035 62.5791 0000592 274.9152 85.1632 15.27589061 01
| Epoch (UTC): | 25 May 2026 11:54:21 |
| Eccentricity: | 0.0000592 |
| inclination: | 43.0035° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 62.5791° |
| argument of perigee: | 274.9152° |
| revolutions per day: | 15.27589061 |
| mean anomaly at epoch: | 85.1632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|