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 00085U 61004C 18170.27152572 .00002638 00000-0 61212-3 0 9996
2 00085 38.7728 135.2504 0387644 328.7170 29.1029 14.18651285827416
| Epoch (UTC): | 19 June 2018 06:30:59 |
| Eccentricity: | 0.0387644 |
| inclination: | 38.7728° |
| perigee height: | 550 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 135.2504° |
| argument of perigee: | 328.7170° |
| revolutions per day: | 14.18651285 |
| mean anomaly at epoch: | 29.1029° |
| orbit number at epoch: | 82741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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