View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47258U 26145.56777378 +.00000000 +00000-0 +11629-2 0 00008
2 47258 87.8951 355.1753 0001502 81.2540 278.8759 13.12443357 02
| Epoch (UTC): | 25 May 2026 13:37:35 |
| Eccentricity: | 0.0001502 |
| inclination: | 87.8951° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1753° |
| argument of perigee: | 81.2540° |
| revolutions per day: | 13.12443357 |
| mean anomaly at epoch: | 278.8759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|