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 15030.84566399 -.00000208 00000-0 -79687-4 0 4774
2 22803 070.9899 279.1397 0019671 269.1803 090.7067 14.16700209105296
| Epoch (UTC): | 30 January 2015 20:17:45 |
| Eccentricity: | 0.0019671 |
| inclination: | 70.9899° |
| perigee height: | 822 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 279.1397° |
| argument of perigee: | 269.1803° |
| revolutions per day: | 14.16700209 |
| mean anomaly at epoch: | 90.7067° |
| orbit number at epoch: | 10529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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