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 43137U 18004AC 23081.75559836 .00040880 00000-0 10315-2 0 9995
2 43137 97.3355 160.3820 0006899 97.3874 262.8156 15.39711831288975
| Epoch (UTC): | 22 March 2023 18:08:03 |
| Eccentricity: | 0.0006899 |
| inclination: | 97.3355° |
| perigee height: | 442 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 160.3820° |
| argument of perigee: | 97.3874° |
| revolutions per day: | 15.39711831 |
| mean anomaly at epoch: | 262.8156° |
| orbit number at epoch: | 28897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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