View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65098U 26145.38549113 +.00000000 +00000-0 +62315-3 0 00003
2 65098 53.1597 29.6099 0001625 92.7552 267.3636 15.34413293 07
| Epoch (UTC): | 25 May 2026 09:15:06 |
| Eccentricity: | 0.0001625 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.6099° |
| argument of perigee: | 92.7552° |
| revolutions per day: | 15.34413293 |
| mean anomaly at epoch: | 267.3636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|