View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66871U 26145.64588153 +.00000000 +00000-0 +55727-3 0 00008
2 66871 42.9975 268.9767 0000761 303.6173 56.4606 15.27615079 08
| Epoch (UTC): | 25 May 2026 15:30:04 |
| Eccentricity: | 0.0000761 |
| inclination: | 42.9975° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 268.9767° |
| argument of perigee: | 303.6173° |
| revolutions per day: | 15.27615079 |
| mean anomaly at epoch: | 56.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|