View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67243U 26145.45749106 +.00000000 +00000-0 +58143-4 0 00004
2 67243 50.0004 197.4167 0001035 246.9637 113.1126 13.29322639 09
| Epoch (UTC): | 25 May 2026 10:58:47 |
| Eccentricity: | 0.0001035 |
| inclination: | 50.0004° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.4167° |
| argument of perigee: | 246.9637° |
| revolutions per day: | 13.29322639 |
| mean anomaly at epoch: | 113.1126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|