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 23030.91072864 .00000042 00000-0 47076-4 0 9991
2 00016 34.2719 269.7757 2027168 315.0874 30.2192 10.48809271559367
| Epoch (UTC): | 30 January 2023 21:51:26 |
| Eccentricity: | 0.2027168 |
| inclination: | 34.2719° |
| perigee height: | 651 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 269.7757° |
| argument of perigee: | 315.0874° |
| revolutions per day: | 10.48809271 |
| mean anomaly at epoch: | 30.2192° |
| orbit number at epoch: | 55936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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