View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65871U 26145.41987785 +.00000000 +00000-0 +65224-3 0 00009
2 65871 53.1608 297.7505 0001370 98.7765 261.3391 15.30217124 01
| Epoch (UTC): | 25 May 2026 10:04:37 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.7505° |
| argument of perigee: | 98.7765° |
| revolutions per day: | 15.30217124 |
| mean anomaly at epoch: | 261.3391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|