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 17145.92630483 +.00000061 +00000-0 +14691-4 0 9994
2 25276 086.3933 296.2840 0002252 093.7245 266.4209 14.34213265002662
| Epoch (UTC): | 25 May 2017 22:13:52 |
| Eccentricity: | 0.0002252 |
| inclination: | 86.3933° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 296.2840° |
| argument of perigee: | 93.7245° |
| revolutions per day: | 14.34213265 |
| mean anomaly at epoch: | 266.4209° |
| orbit number at epoch: | 266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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