View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65900U 26145.05867737 +.00000000 +00000-0 +90498-3 0 00007
2 65900 53.1595 15.4193 0001092 98.1216 261.9911 15.34416714 07
| Epoch (UTC): | 25 May 2026 01:24:29 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 15.4193° |
| argument of perigee: | 98.1216° |
| revolutions per day: | 15.34416714 |
| mean anomaly at epoch: | 261.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|