View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54071U 26145.29507073 +.00000000 +00000-0 +40400-4 0 00003
2 54071 53.2146 359.8789 0001238 85.4854 274.6280 15.08833160 01
| Epoch (UTC): | 25 May 2026 07:04:54 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 359.8789° |
| argument of perigee: | 85.4854° |
| revolutions per day: | 15.08833160 |
| mean anomaly at epoch: | 274.6280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|