View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67655U 26145.55222050 +.00000000 +00000-0 +37420-3 0 00000
2 67655 97.2855 178.8278 0000644 104.8681 255.2634 15.33448990 03
| Epoch (UTC): | 25 May 2026 13:15:11 |
| Eccentricity: | 0.0000644 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.8278° |
| argument of perigee: | 104.8681° |
| revolutions per day: | 15.33448990 |
| mean anomaly at epoch: | 255.2634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|