View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65329U 26145.41336796 +.00000000 +00000-0 +38525-3 0 00001
2 65329 53.1575 210.3598 0001028 79.4420 280.6696 15.30205651 03
| Epoch (UTC): | 25 May 2026 09:55:14 |
| Eccentricity: | 0.0001028 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.3598° |
| argument of perigee: | 79.4420° |
| revolutions per day: | 15.30205651 |
| mean anomaly at epoch: | 280.6696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|