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 23029.95803746 .00000041 00000-0 43119-4 0 9997
2 00016 34.2730 272.5267 2027251 311.0704 33.1299 10.48809255559260
| Epoch (UTC): | 29 January 2023 22:59:34 |
| Eccentricity: | 0.2027251 |
| inclination: | 34.2730° |
| perigee height: | 650 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 272.5267° |
| argument of perigee: | 311.0704° |
| revolutions per day: | 10.48809255 |
| mean anomaly at epoch: | 33.1299° |
| orbit number at epoch: | 55926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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