View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67802U 26145.25174571 +.00000000 +00000-0 +55664-3 0 00005
2 67802 97.2855 333.3385 0001844 102.2292 257.9157 15.33470696 04
| Epoch (UTC): | 25 May 2026 06:02:30 |
| Eccentricity: | 0.0001844 |
| inclination: | 97.2855° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.3385° |
| argument of perigee: | 102.2292° |
| revolutions per day: | 15.33470696 |
| mean anomaly at epoch: | 257.9157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|