View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63998U 26145.65561601 +.00000000 +00000-0 +81883-3 0 00007
2 63998 42.9983 283.5242 0001410 262.5744 97.4947 15.27594670 00
| Epoch (UTC): | 25 May 2026 15:44:05 |
| Eccentricity: | 0.0001410 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.5242° |
| argument of perigee: | 262.5744° |
| revolutions per day: | 15.27594670 |
| mean anomaly at epoch: | 97.4947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|