View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43229U 26145.15802277 +.00000000 +00000-0 +71089-3 0 00001
2 43229 26.8137 170.0244 3497876 36.9889 342.7127 8.53877009 07
| Epoch (UTC): | 25 May 2026 03:47:33 |
| Eccentricity: | 0.3497876 |
| inclination: | 26.8137° |
| perigee height: | 196 km |
| apogee height: | 7270 km |
| right ascension of ascending node: | 170.0244° |
| argument of perigee: | 36.9889° |
| revolutions per day: | 8.53877009 |
| mean anomaly at epoch: | 342.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|