View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26958U 26145.56777360 +.00000000 +00000-0 +15842-3 0 00005
2 26958 97.9602 153.3122 0054489 198.1182 161.8105 15.07392790 07
| Epoch (UTC): | 25 May 2026 13:37:35 |
| Eccentricity: | 0.0054489 |
| inclination: | 97.9602° |
| perigee height: | 506 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 153.3122° |
| argument of perigee: | 198.1182° |
| revolutions per day: | 15.07392790 |
| mean anomaly at epoch: | 161.8105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|