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 23026.05217142 .00000089 00000-0 10348-3 0 9993
2 00016 34.2769 283.8036 2027559 294.6062 45.6951 10.48809168558855
| Epoch (UTC): | 26 January 2023 01:15:07 |
| Eccentricity: | 0.2027559 |
| inclination: | 34.2769° |
| perigee height: | 650 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 283.8036° |
| argument of perigee: | 294.6062° |
| revolutions per day: | 10.48809168 |
| mean anomaly at epoch: | 45.6951° |
| orbit number at epoch: | 55885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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