View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65147U 26145.46153951 +.00000000 +00000-0 +29043-3 0 00009
2 65147 51.9007 176.0812 0000385 58.3278 301.7722 14.79931068 01
| Epoch (UTC): | 25 May 2026 11:04:37 |
| Eccentricity: | 0.0000385 |
| inclination: | 51.9007° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 176.0812° |
| argument of perigee: | 58.3278° |
| revolutions per day: | 14.79931068 |
| mean anomaly at epoch: | 301.7722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|