View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00059U 26131.77220514 +.00000000 +00000-0 +24800-4 0 00006
2 00059 28.2501 310.6395 0188906 10.0989 350.3282 13.53168233 08
| Epoch (UTC): | 11 May 2026 18:31:58 |
| Eccentricity: | 0.0188906 |
| inclination: | 28.2501° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 310.6395° |
| argument of perigee: | 10.0989° |
| revolutions per day: | 13.53168233 |
| mean anomaly at epoch: | 350.3282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|