View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66302U 26145.02136441 +.00000000 +00000-0 +24875-3 0 00008
2 66302 45.4050 255.1199 0007617 262.8934 97.1082 15.08838177 09
| Epoch (UTC): | 25 May 2026 00:30:45 |
| Eccentricity: | 0.0007617 |
| inclination: | 45.4050° |
| perigee height: | 534 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 255.1199° |
| argument of perigee: | 262.8934° |
| revolutions per day: | 15.08838177 |
| mean anomaly at epoch: | 97.1082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|