View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65127U 26145.62031549 +.00000000 +00000-0 +19468-3 0 00003
2 65127 49.9926 308.1705 0021947 304.1989 55.6868 14.81298004 08
| Epoch (UTC): | 25 May 2026 14:53:15 |
| Eccentricity: | 0.0021947 |
| inclination: | 49.9926° |
| perigee height: | 610 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 308.1705° |
| argument of perigee: | 304.1989° |
| revolutions per day: | 14.81298004 |
| mean anomaly at epoch: | 55.6868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|