View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66283U 26145.51127367 +.00000000 +00000-0 +46412-3 0 00008
2 66283 53.1579 194.7357 0001185 53.4093 306.7016 15.30207988 08
| Epoch (UTC): | 25 May 2026 12:16:14 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.7357° |
| argument of perigee: | 53.4093° |
| revolutions per day: | 15.30207988 |
| mean anomaly at epoch: | 306.7016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|