View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63506U 26145.37515914 +.00000000 +00000-0 +40247-3 0 00006
2 63506 53.1581 143.5259 0001147 80.5702 279.5428 15.30205681 07
| Epoch (UTC): | 25 May 2026 09:00:13 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5259° |
| argument of perigee: | 80.5702° |
| revolutions per day: | 15.30205681 |
| mean anomaly at epoch: | 279.5428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|