View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64285U 26145.63954779 +.00000000 +00000-0 +37224-4 0 00008
2 64285 86.4970 21.0198 0001671 83.7602 276.3722 13.24407973 02
| Epoch (UTC): | 25 May 2026 15:20:56 |
| Eccentricity: | 0.0001671 |
| inclination: | 86.4970° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.0198° |
| argument of perigee: | 83.7602° |
| revolutions per day: | 13.24407973 |
| mean anomaly at epoch: | 276.3722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|