View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65133U 26145.41699178 +.00000000 +00000-0 +30439-3 0 00006
2 65133 51.8981 186.2899 0000256 51.6672 308.4314 14.79935564 01
| Epoch (UTC): | 25 May 2026 10:00:28 |
| Eccentricity: | 0.0000256 |
| inclination: | 51.8981° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 186.2899° |
| argument of perigee: | 51.6672° |
| revolutions per day: | 14.79935564 |
| mean anomaly at epoch: | 308.4314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|