View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65369U 26145.49385367 +.00000000 +00000-0 +41319-3 0 00006
2 65369 53.1580 171.4753 0001109 90.1352 269.9776 15.30206920 06
| Epoch (UTC): | 25 May 2026 11:51:08 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.4753° |
| argument of perigee: | 90.1352° |
| revolutions per day: | 15.30206920 |
| mean anomaly at epoch: | 269.9776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|