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 is defined by the following mean orbital elements,
1 42296U 95015HN 16156.79985534 .00001840 00000-0 92551-3 0 9990
2 42296 98.8071 160.8571 0016628 53.4994 306.8117 14.17605117 37541
| Epoch (UTC): | 04 June 2016 19:11:47 |
| Eccentricity: | 0.0016628 |
| inclination: | 98.8071° |
| perigee height: | 821 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 160.8571° |
| argument of perigee: | 53.4994° |
| revolutions per day: | 14.17605117 |
| mean anomaly at epoch: | 306.8117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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