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 18267.39554254 -.00000003 +00000-0 -15434-2 0 9997
2 1002 032.1413 251.8054 0015373 148.3437 211.7987 09.88353059936905
| Epoch (UTC): | 24 September 2018 09:29:34 |
| Eccentricity: | 0.0015373 |
| inclination: | 32.1413° |
| perigee height: | 2779 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 251.8054° |
| argument of perigee: | 148.3437° |
| revolutions per day: | 9.88353059 |
| mean anomaly at epoch: | 211.7987° |
| orbit number at epoch: | 93690 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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