View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65099U 26145.05349750 +.00000000 +00000-0 +36380-3 0 00006
2 65099 53.1589 31.0920 0000945 118.5713 241.5385 15.34400640 06
| Epoch (UTC): | 25 May 2026 01:17:02 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 31.0920° |
| argument of perigee: | 118.5713° |
| revolutions per day: | 15.34400640 |
| mean anomaly at epoch: | 241.5385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|