View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58140U 26145.47980442 +.00000000 +00000-0 -69668-4 0 00007
2 58140 42.9992 58.6000 0000872 63.3129 296.7811 15.27581455 02
| Epoch (UTC): | 25 May 2026 11:30:55 |
| Eccentricity: | 0.0000872 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.6000° |
| argument of perigee: | 63.3129° |
| revolutions per day: | 15.27581455 |
| mean anomaly at epoch: | 296.7811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|