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 23038.53262951 .00000106 00000-0 15173-3 0 9998
2 00016 34.2638 247.7609 2026606 347.2341 8.3496 10.48810422560164
| Epoch (UTC): | 07 February 2023 12:46:59 |
| Eccentricity: | 0.2026606 |
| inclination: | 34.2638° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 247.7609° |
| argument of perigee: | 347.2341° |
| revolutions per day: | 10.48810422 |
| mean anomaly at epoch: | 8.3496° |
| orbit number at epoch: | 56016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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