View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00059U 26037.26770705 +.00000000 +00000-0 +86699-4 0 00001
2 00059 28.2499 76.2391 0188858 296.7295 61.4037 13.53160728 03
| Epoch (UTC): | 06 February 2026 06:25:29 |
| Eccentricity: | 0.0188858 |
| inclination: | 28.2499° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 76.2391° |
| argument of perigee: | 296.7295° |
| revolutions per day: | 13.53160728 |
| mean anomaly at epoch: | 61.4037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|