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 19197.50795360 .00000101 00000-0 18831-4 0 9996
2 29678 90.0352 18.3546 0203856 64.9344 297.2867 14.44287032649650
| Epoch (UTC): | 16 July 2019 12:11:27 |
| Eccentricity: | 0.0203856 |
| inclination: | 90.0352° |
| perigee height: | 599 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 18.3546° |
| argument of perigee: | 64.9344° |
| revolutions per day: | 14.44287032 |
| mean anomaly at epoch: | 297.2867° |
| orbit number at epoch: | 64965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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