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 00016U 58002A 23089.10334839 .00000118 00000-0 14438-3 0 9998
2 00016 34.2660 101.6697 2025475 200.5400 150.0679 10.48820712565474
| Epoch (UTC): | 30 March 2023 02:28:49 |
| Eccentricity: | 0.2025475 |
| inclination: | 34.2660° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 101.6697° |
| argument of perigee: | 200.5400° |
| revolutions per day: | 10.48820712 |
| mean anomaly at epoch: | 150.0679° |
| orbit number at epoch: | 56547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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