View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60592U 26145.43853050 +.00000000 +00000-0 +23938-4 0 00000
2 60592 53.1602 309.7091 0001146 92.6023 267.5111 15.34389119 01
| Epoch (UTC): | 25 May 2026 10:31:29 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.7091° |
| argument of perigee: | 92.6023° |
| revolutions per day: | 15.34389119 |
| mean anomaly at epoch: | 267.5111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|