View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66933U 26145.33119183 +.00000000 +00000-0 +12704-2 0 00003
2 66933 53.1619 2.2622 0001172 101.5712 258.5422 15.34456585 00
| Epoch (UTC): | 25 May 2026 07:56:54 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.1619° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 2.2622° |
| argument of perigee: | 101.5712° |
| revolutions per day: | 15.34456585 |
| mean anomaly at epoch: | 258.5422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|