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 25276U 98019E 17206.20631489 +.00000140 +00000-0 +42878-4 0 9996
2 25276 086.3952 271.0796 0002290 093.9950 266.1508 14.34219137011305
| Epoch (UTC): | 25 July 2017 04:57:05 |
| Eccentricity: | 0.0002290 |
| inclination: | 86.3952° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 271.0796° |
| argument of perigee: | 93.9950° |
| revolutions per day: | 14.34219137 |
| mean anomaly at epoch: | 266.1508° |
| orbit number at epoch: | 1130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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