View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67686U 26145.02823793 +.00000000 +00000-0 +76375-3 0 00009
2 67686 51.6280 49.4172 0009892 99.7190 260.4921 15.61190741 06
| Epoch (UTC): | 25 May 2026 00:40:39 |
| Eccentricity: | 0.0009892 |
| inclination: | 51.6280° |
| perigee height: | 378 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 49.4172° |
| argument of perigee: | 99.7190° |
| revolutions per day: | 15.61190741 |
| mean anomaly at epoch: | 260.4921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|