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 40014U 14033E 23091.26980554 .00007072 00000-0 58654-3 0 9991
2 40014 98.1463 106.8092 0030096 159.4336 200.8106 14.98790536479219
| Epoch (UTC): | 01 April 2023 06:28:31 |
| Eccentricity: | 0.0030096 |
| inclination: | 98.1463° |
| perigee height: | 550 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 106.8092° |
| argument of perigee: | 159.4336° |
| revolutions per day: | 14.98790536 |
| mean anomaly at epoch: | 200.8106° |
| orbit number at epoch: | 47921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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