View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39420U 26145.10330605 +.00000000 +00000-0 +17118-3 0 00008
2 39420 97.6837 11.2233 0118210 85.9812 275.4899 14.72255434 09
| Epoch (UTC): | 25 May 2026 02:28:45 |
| Eccentricity: | 0.0118210 |
| inclination: | 97.6837° |
| perigee height: | 571 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 11.2233° |
| argument of perigee: | 85.9812° |
| revolutions per day: | 14.72255434 |
| mean anomaly at epoch: | 275.4899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|