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 1002U 65008C 18347.54860992 -.00000007 +00000-0 -19762-2 0 9994
2 1002 032.1465 061.9121 0015102 076.5928 283.6252 09.88352890944830
| Epoch (UTC): | 13 December 2018 13:09:59 |
| Eccentricity: | 0.0015102 |
| inclination: | 32.1465° |
| perigee height: | 2780 km |
| apogee height: | 2807 km |
| right ascension of ascending node: | 61.9121° |
| argument of perigee: | 76.5928° |
| revolutions per day: | 9.88352890 |
| mean anomaly at epoch: | 283.6252° |
| orbit number at epoch: | 94483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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