View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67736U 26145.14026091 +.00000000 +00000-0 +51737-3 0 00009
2 67736 97.2847 198.6869 0000921 85.4681 274.6667 15.33435579 02
| Epoch (UTC): | 25 May 2026 03:21:58 |
| Eccentricity: | 0.0000921 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.6869° |
| argument of perigee: | 85.4681° |
| revolutions per day: | 15.33435579 |
| mean anomaly at epoch: | 274.6667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|