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 10489U 77108A 18350.40742652 -.00000152 00000-0 00000+0 0 9990
2 10489 11.4565 314.1236 0015537 7.1031 353.4000 1.00160431109785
| Epoch (UTC): | 16 December 2018 09:46:41 |
| Eccentricity: | 0.0015537 |
| inclination: | 11.4565° |
| perigee height: | 35752 km |
| apogee height: | 35883 km |
| right ascension of ascending node: | 314.1236° |
| argument of perigee: | 7.1031° |
| revolutions per day: | 1.00160431 |
| mean anomaly at epoch: | 353.4000° |
| orbit number at epoch: | 10978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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