View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65601U 26145.14702218 +.00000000 +00000-0 -44928-4 0 00006
2 65601 97.4500 213.6230 0001584 132.2770 227.8592 15.05647981 03
| Epoch (UTC): | 25 May 2026 03:31:42 |
| Eccentricity: | 0.0001584 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.6230° |
| argument of perigee: | 132.2770° |
| revolutions per day: | 15.05647981 |
| mean anomaly at epoch: | 227.8592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|