View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66462U 26145.54400563 +.00000000 +00000-0 +37095-3 0 00009
2 66462 43.0048 221.8546 0003085 283.6342 76.4166 15.27581933 01
| Epoch (UTC): | 25 May 2026 13:03:22 |
| Eccentricity: | 0.0003085 |
| inclination: | 43.0048° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 221.8546° |
| argument of perigee: | 283.6342° |
| revolutions per day: | 15.27581933 |
| mean anomaly at epoch: | 76.4166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|