View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68133U 26145.34136458 +.00000000 +00000-0 +85107-4 0 00001
2 68133 49.9995 138.0246 0000436 3.7712 356.3163 13.29330744 08
| Epoch (UTC): | 25 May 2026 08:11:33 |
| Eccentricity: | 0.0000436 |
| inclination: | 49.9995° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 138.0246° |
| argument of perigee: | 3.7712° |
| revolutions per day: | 13.29330744 |
| mean anomaly at epoch: | 356.3163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|