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 29678U 06063A 19045.98230843 .00000099 00000-0 19558-4 0 9993
2 29678 90.0371 17.6662 0200125 216.8671 141.8637 14.44245762627782
| Epoch (UTC): | 14 February 2019 23:34:31 |
| Eccentricity: | 0.0200125 |
| inclination: | 90.0371° |
| perigee height: | 602 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 17.6662° |
| argument of perigee: | 216.8671° |
| revolutions per day: | 14.44245762 |
| mean anomaly at epoch: | 141.8637° |
| orbit number at epoch: | 62778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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