View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66285U 26145.43645980 +.00000000 +00000-0 +41008-3 0 00003
2 66285 53.1590 194.9806 0001300 90.3560 269.7590 15.30204238 02
| Epoch (UTC): | 25 May 2026 10:28:30 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.9806° |
| argument of perigee: | 90.3560° |
| revolutions per day: | 15.30204238 |
| mean anomaly at epoch: | 269.7590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|