View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62554U 26145.41683530 +.00000000 +00000-0 +20891-2 0 00005
2 62554 43.0008 37.0486 0002074 63.9446 296.1635 15.70896433 00
| Epoch (UTC): | 25 May 2026 10:00:14 |
| Eccentricity: | 0.0002074 |
| inclination: | 43.0008° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 37.0486° |
| argument of perigee: | 63.9446° |
| revolutions per day: | 15.70896433 |
| mean anomaly at epoch: | 296.1635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|