View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68092U 26145.36824668 +.00000000 +00000-0 +79633-3 0 00000
2 68092 53.1596 181.9463 0001213 80.2165 279.8974 15.34402444 04
| Epoch (UTC): | 25 May 2026 08:50:16 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.9463° |
| argument of perigee: | 80.2165° |
| revolutions per day: | 15.34402444 |
| mean anomaly at epoch: | 279.8974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|