View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65639U 26145.48473175 +.00000000 +00000-0 +11636-2 0 00008
2 65639 53.1587 309.3173 0001501 83.9336 276.1837 15.34424356 06
| Epoch (UTC): | 25 May 2026 11:38:00 |
| Eccentricity: | 0.0001501 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.3173° |
| argument of perigee: | 83.9336° |
| revolutions per day: | 15.34424356 |
| mean anomaly at epoch: | 276.1837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|