View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58388U 26144.93257455 +.00000000 +00000-0 +92940-4 0 00000
2 58388 53.1615 6.2896 0001399 84.4158 275.7004 15.34397871 01
| Epoch (UTC): | 24 May 2026 22:22:54 |
| Eccentricity: | 0.0001399 |
| inclination: | 53.1615° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 6.2896° |
| argument of perigee: | 84.4158° |
| revolutions per day: | 15.34397871 |
| mean anomaly at epoch: | 275.7004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|