View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59433U 26145.11119476 +.00000000 +00000-0 +35764-6 0 00006
2 59433 53.1602 288.5699 0000748 107.8934 252.2149 15.30195155 01
| Epoch (UTC): | 25 May 2026 02:40:07 |
| Eccentricity: | 0.0000748 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.5699° |
| argument of perigee: | 107.8934° |
| revolutions per day: | 15.30195155 |
| mean anomaly at epoch: | 252.2149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|