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 23027.00479396 .00000071 00000-0 80120-4 0 9997
2 00016 34.2762 281.0533 2027498 298.6211 42.5260 10.48809206558955
| Epoch (UTC): | 27 January 2023 00:06:54 |
| Eccentricity: | 0.2027498 |
| inclination: | 34.2762° |
| perigee height: | 650 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 281.0533° |
| argument of perigee: | 298.6211° |
| revolutions per day: | 10.48809206 |
| mean anomaly at epoch: | 42.5260° |
| orbit number at epoch: | 55895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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