View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61208U 26145.41970747 +.00000000 +00000-0 -46572-5 0 00007
2 61208 53.1566 157.7454 0000702 83.9272 276.1826 15.69716997 00
| Epoch (UTC): | 25 May 2026 10:04:22 |
| Eccentricity: | 0.0000702 |
| inclination: | 53.1566° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 157.7454° |
| argument of perigee: | 83.9272° |
| revolutions per day: | 15.69716997 |
| mean anomaly at epoch: | 276.1826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|