View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67529U 26145.54670465 +.00000000 +00000-0 +73990-4 0 00009
2 67529 50.0045 76.5318 0000918 29.0215 331.0708 13.29327941 05
| Epoch (UTC): | 25 May 2026 13:07:15 |
| Eccentricity: | 0.0000918 |
| inclination: | 50.0045° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 76.5318° |
| argument of perigee: | 29.0215° |
| revolutions per day: | 13.29327941 |
| mean anomaly at epoch: | 331.0708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|