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 59U 60013B 19145.18405252 .00000078 00000-0 -16775-4 0 9997
2 59 28.2508 57.7761 0189268 258.9362 98.9844 13.52968344894359
| Epoch (UTC): | 25 May 2019 04:25:02 |
| Eccentricity: | 0.0189268 |
| inclination: | 28.2508° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 57.7761° |
| argument of perigee: | 258.9362° |
| revolutions per day: | 13.52968344 |
| mean anomaly at epoch: | 98.9844° |
| orbit number at epoch: | 89435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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