View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58765U 26144.93713699 +.00000000 +00000-0 -20605-4 0 00006
2 58765 53.1617 19.5502 0001255 84.6331 275.4813 15.30204759 02
| Epoch (UTC): | 24 May 2026 22:29:28 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 19.5502° |
| argument of perigee: | 84.6331° |
| revolutions per day: | 15.30204759 |
| mean anomaly at epoch: | 275.4813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|