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 19884U 89021C 16270.00581654 .00010689 00000-0 91668-3 0 9992
2 19884 26.4345 210.4718 5986484 319.2382 8.7240 4.10170963323089
| Epoch (UTC): | 26 September 2016 00:08:22 |
| Eccentricity: | 0.5986484 |
| inclination: | 26.4345° |
| perigee height: | 238 km |
| apogee height: | 19975 km |
| right ascension of ascending node: | 210.4718° |
| argument of perigee: | 319.2382° |
| revolutions per day: | 4.10170963 |
| mean anomaly at epoch: | 8.7240° |
| orbit number at epoch: | 32308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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