View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00085U 61004C 22176.45252406 .00002644 00000-0 53282-3 0 9999
2 00085 38.7654 205.2454 0371794 32.9979 329.3398 14.26971738 36228
| Epoch (UTC): | 25 June 2022 10:51:38 |
| Eccentricity: | 0.0371794 |
| inclination: | 38.7654° |
| perigee height: | 535 km |
| apogee height: | 1069 km |
| right ascension of ascending node: | 205.2454° |
| argument of perigee: | 32.9979° |
| revolutions per day: | 14.26971738 |
| mean anomaly at epoch: | 329.3398° |
| orbit number at epoch: | 3622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|