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 40028U 14033U 19082.76454074 .00000433 00000-0 52370-4 0 9993
2 40028 97.9112 3.0933 0013740 351.6730 8.4261 14.88733095258366
| Epoch (UTC): | 23 March 2019 18:20:56 |
| Eccentricity: | 0.0013740 |
| inclination: | 97.9112° |
| perigee height: | 592 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 3.0933° |
| argument of perigee: | 351.6730° |
| revolutions per day: | 14.88733095 |
| mean anomaly at epoch: | 8.4261° |
| orbit number at epoch: | 25836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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