View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60590U 26145.42382385 +.00000000 +00000-0 +54081-5 0 00009
2 60590 53.1618 309.6112 0000989 95.8950 264.2165 15.34378570 09
| Epoch (UTC): | 25 May 2026 10:10:18 |
| Eccentricity: | 0.0000989 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.6112° |
| argument of perigee: | 95.8950° |
| revolutions per day: | 15.34378570 |
| mean anomaly at epoch: | 264.2165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|