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 24357.55095170 .00000284 00000-0 39833-3 0 9998
2 00016 34.2677 71.4706 2023320 353.2096 4.4535 10.49511559632005
| Epoch (UTC): | 22 December 2024 13:13:22 |
| Eccentricity: | 0.2023320 |
| inclination: | 34.2677° |
| perigee height: | 651 km |
| apogee height: | 4217 km |
| right ascension of ascending node: | 71.4706° |
| argument of perigee: | 353.2096° |
| revolutions per day: | 10.49511559 |
| mean anomaly at epoch: | 4.4535° |
| orbit number at epoch: | 63200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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