View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65865U 26145.13119134 +.00000000 +00000-0 +67823-3 0 00003
2 65865 53.1595 298.7946 0001187 90.3661 269.7476 15.30207033 02
| Epoch (UTC): | 25 May 2026 03:08:54 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.7946° |
| argument of perigee: | 90.3661° |
| revolutions per day: | 15.30207033 |
| mean anomaly at epoch: | 269.7476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|