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 43445U 18036E 23273.06944358 .00000004 00000-0 00000-0 0 9998
2 43445 4.6775 78.4480 0009621 127.4033 201.0055 1.02112032 16811
| Epoch (UTC): | 30 September 2023 01:39:59 |
| Eccentricity: | 0.0009621 |
| inclination: | 4.6775° |
| perigee height: | 35238 km |
| apogee height: | 35318 km |
| right ascension of ascending node: | 78.4480° |
| argument of perigee: | 127.4033° |
| revolutions per day: | 1.02112032 |
| mean anomaly at epoch: | 201.0055° |
| orbit number at epoch: | 1681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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