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 19287.49403616 +.00000003 +00000-0 -69562-3 0 9997
2 1002 032.1460 059.4945 0014031 099.3930 260.8154 09.88353436975005
| Epoch (UTC): | 14 October 2019 11:51:24 |
| Eccentricity: | 0.0014031 |
| inclination: | 32.1460° |
| perigee height: | 2781 km |
| apogee height: | 2806 km |
| right ascension of ascending node: | 59.4945° |
| argument of perigee: | 99.3930° |
| revolutions per day: | 9.88353436 |
| mean anomaly at epoch: | 260.8154° |
| orbit number at epoch: | 97500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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