View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63836U 26145.01482485 +.00000000 +00000-0 +17886-3 0 00002
2 63836 43.0065 6.9939 0002224 286.1163 73.9444 15.27582853 06
| Epoch (UTC): | 25 May 2026 00:21:20 |
| Eccentricity: | 0.0002224 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 6.9939° |
| argument of perigee: | 286.1163° |
| revolutions per day: | 15.27582853 |
| mean anomaly at epoch: | 73.9444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|