View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28352U 04021A 16270.49556598 -.00000177 00000-0 -71686-4 0 9993
2 28352 71.0014 315.2587 0013771 143.8656 216.3398 14.11443814633632
| Epoch (UTC): | 26 September 2016 11:53:36 |
| Eccentricity: | 0.0013771 |
| inclination: | 71.0014° |
| perigee height: | 844 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 315.2587° |
| argument of perigee: | 143.8656° |
| revolutions per day: | 14.11443814 |
| mean anomaly at epoch: | 216.3398° |
| orbit number at epoch: | 63363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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