View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67203U 26145.26122193 +.00000000 +00000-0 +14379-3 0 00002
2 67203 70.0013 341.4161 0002479 265.2190 94.8686 14.98334069 06
| Epoch (UTC): | 25 May 2026 06:16:09 |
| Eccentricity: | 0.0002479 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.4161° |
| argument of perigee: | 265.2190° |
| revolutions per day: | 14.98334069 |
| mean anomaly at epoch: | 94.8686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|