View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67738U 26145.13207758 +.00000000 +00000-0 +45208-3 0 00007
2 67738 97.2848 198.6990 0000830 118.5757 241.5569 15.33486469 09
| Epoch (UTC): | 25 May 2026 03:10:11 |
| Eccentricity: | 0.0000830 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.6990° |
| argument of perigee: | 118.5757° |
| revolutions per day: | 15.33486469 |
| mean anomaly at epoch: | 241.5569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|