View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67903U 26145.34144625 +.00000000 +00000-0 +45132-3 0 00003
2 67903 97.2852 78.8423 0001716 99.2537 260.8900 15.33447376 00
| Epoch (UTC): | 25 May 2026 08:11:40 |
| Eccentricity: | 0.0001716 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.8423° |
| argument of perigee: | 99.2537° |
| revolutions per day: | 15.33447376 |
| mean anomaly at epoch: | 260.8900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|