View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68439U 26145.13192958 +.00000000 +00000-0 +57305-3 0 00002
2 68439 97.4502 103.9290 0004717 116.6181 243.5537 15.18790835 02
| Epoch (UTC): | 25 May 2026 03:09:58 |
| Eccentricity: | 0.0004717 |
| inclination: | 97.4502° |
| perigee height: | 506 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 103.9290° |
| argument of perigee: | 116.6181° |
| revolutions per day: | 15.18790835 |
| mean anomaly at epoch: | 243.5537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|