View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51951U 26145.61469850 +.00000000 +00000-0 +72244-3 0 00003
2 51951 63.4470 350.2214 0128374 343.6081 16.0896 15.18017828 05
| Epoch (UTC): | 25 May 2026 14:45:09 |
| Eccentricity: | 0.0128374 |
| inclination: | 63.4470° |
| perigee height: | 423 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 350.2214° |
| argument of perigee: | 343.6081° |
| revolutions per day: | 15.18017828 |
| mean anomaly at epoch: | 16.0896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|