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 23088.72257760 .00000122 00000-0 15060-3 0 9999
2 00016 34.2656 102.7696 2025471 198.9337 152.3710 10.48820652565435
| Epoch (UTC): | 29 March 2023 17:20:30 |
| Eccentricity: | 0.2025471 |
| inclination: | 34.2656° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 102.7696° |
| argument of perigee: | 198.9337° |
| revolutions per day: | 10.48820652 |
| mean anomaly at epoch: | 152.3710° |
| orbit number at epoch: | 56543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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