View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 5485U 71080A 18267.61436297 +.00000016 +00000-0 +16555-5 0 9994
2 5485 032.0532 074.7540 0639653 098.7366 268.6163 12.74126864189097
| Epoch (UTC): | 24 September 2018 14:44:40 |
| Eccentricity: | 0.0639653 |
| inclination: | 32.0532° |
| perigee height: | 870 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 74.7540° |
| argument of perigee: | 98.7366° |
| revolutions per day: | 12.74126864 |
| mean anomaly at epoch: | 268.6163° |
| orbit number at epoch: | 18909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|