View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58549U 26145.49765270 +.00000000 +00000-0 +17283-3 0 00006
2 58549 53.1609 65.3672 0000930 92.8532 267.2577 15.34389794 06
| Epoch (UTC): | 25 May 2026 11:56:37 |
| Eccentricity: | 0.0000930 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.3672° |
| argument of perigee: | 92.8532° |
| revolutions per day: | 15.34389794 |
| mean anomaly at epoch: | 267.2577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|