View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51722U 26145.55225106 +.00000000 +00000-0 -96915-5 0 00000
2 51722 53.2136 344.0686 0001063 84.9305 275.1809 15.08836584 09
| Epoch (UTC): | 25 May 2026 13:15:14 |
| Eccentricity: | 0.0001063 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 344.0686° |
| argument of perigee: | 84.9305° |
| revolutions per day: | 15.08836584 |
| mean anomaly at epoch: | 275.1809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|