View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66115U 26145.14270139 +.00000000 +00000-0 +64091-3 0 00000
2 66115 53.1588 44.6651 0001049 85.7683 274.3438 15.30191958 01
| Epoch (UTC): | 25 May 2026 03:25:29 |
| Eccentricity: | 0.0001049 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.6651° |
| argument of perigee: | 85.7683° |
| revolutions per day: | 15.30191958 |
| mean anomaly at epoch: | 274.3438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|