View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63361U 26145.45699353 +.00000000 +00000-0 +00000-0 0 00004
2 63361 4.4311 274.7685 0031969 11.2028 201.6809 1.00271520 09
| Epoch (UTC): | 25 May 2026 10:58:04 |
| Eccentricity: | 0.0031969 |
| inclination: | 4.4311° |
| perigee height: | 35652 km |
| apogee height: | 35921 km |
| right ascension of ascending node: | 274.7685° |
| argument of perigee: | 11.2028° |
| revolutions per day: | 1.00271520 |
| mean anomaly at epoch: | 201.6809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|