View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67481U 26145.22028725 +.00000000 +00000-0 +21992-3 0 00001
2 67481 41.4769 97.6571 0011371 195.4530 164.5965 15.67799502 01
| Epoch (UTC): | 25 May 2026 05:17:12 |
| Eccentricity: | 0.0011371 |
| inclination: | 41.4769° |
| perigee height: | 358 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 97.6571° |
| argument of perigee: | 195.4530° |
| revolutions per day: | 15.67799502 |
| mean anomaly at epoch: | 164.5965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|