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 22803U 93059B 16270.51790362 .00000220 00000-0 13395-3 0 9998
2 22803 70.9888 85.0398 0015239 63.8048 296.4640 14.16753955190938
| Epoch (UTC): | 26 September 2016 12:25:46 |
| Eccentricity: | 0.0015239 |
| inclination: | 70.9888° |
| perigee height: | 825 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 85.0398° |
| argument of perigee: | 63.8048° |
| revolutions per day: | 14.16753955 |
| mean anomaly at epoch: | 296.4640° |
| orbit number at epoch: | 19093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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