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 43145U 18005A 23253.09210970 0.00000000 00000-0 00000-0 0 07
2 43145 105.9939 178.2628 0000540 85.5715 274.4285 13.48029098 05
| Epoch (UTC): | 10 September 2023 02:12:38 |
| Eccentricity: | 0.0000540 |
| inclination: | 105.9939° |
| perigee height: | 1079 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 178.2628° |
| argument of perigee: | 85.5715° |
| revolutions per day: | 13.48029098 |
| mean anomaly at epoch: | 274.4285° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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