View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63747U 26145.61877054 +.00000000 +00000-0 +85236-4 0 00004
2 63747 51.9022 107.9270 0000671 68.2697 291.8337 14.79945420 04
| Epoch (UTC): | 25 May 2026 14:51:01 |
| Eccentricity: | 0.0000671 |
| inclination: | 51.9022° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 107.9270° |
| argument of perigee: | 68.2697° |
| revolutions per day: | 14.79945420 |
| mean anomaly at epoch: | 291.8337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|