View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00059U 26133.61665457 +.00000000 +00000-0 +21695-4 0 00009
2 00059 28.2496 301.1621 0188894 25.5852 335.3907 13.53168250 00
| Epoch (UTC): | 13 May 2026 14:47:58 |
| Eccentricity: | 0.0188894 |
| inclination: | 28.2496° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 301.1621° |
| argument of perigee: | 25.5852° |
| revolutions per day: | 13.53168250 |
| mean anomaly at epoch: | 335.3907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|