View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67887U 26145.38766771 +.00000000 +00000-0 +56863-3 0 00003
2 67887 97.2849 78.9325 0001687 99.0087 261.1347 15.33444892 03
| Epoch (UTC): | 25 May 2026 09:18:14 |
| Eccentricity: | 0.0001687 |
| inclination: | 97.2849° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9325° |
| argument of perigee: | 99.0087° |
| revolutions per day: | 15.33444892 |
| mean anomaly at epoch: | 261.1347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|