View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65142U 26145.56013610 +.00000000 +00000-0 +28396-4 0 00003
2 65142 51.8997 178.1246 0000315 75.6926 284.4072 14.79929777 01
| Epoch (UTC): | 25 May 2026 13:26:35 |
| Eccentricity: | 0.0000315 |
| inclination: | 51.8997° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 178.1246° |
| argument of perigee: | 75.6926° |
| revolutions per day: | 14.79929777 |
| mean anomaly at epoch: | 284.4072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|