View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65183U 26145.14580647 +.00000000 +00000-0 +22237-3 0 00008
2 65183 97.4501 17.6216 0002620 83.6615 276.4911 15.05659894 05
| Epoch (UTC): | 25 May 2026 03:29:57 |
| Eccentricity: | 0.0002620 |
| inclination: | 97.4501° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6216° |
| argument of perigee: | 83.6615° |
| revolutions per day: | 15.05659894 |
| mean anomaly at epoch: | 276.4911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|