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 is defined by the following mean orbital elements,
1 43737U 18096U 23136.75304770 .14838938 24870-5 26605-3 0 9998
2 43737 97.3113 234.2974 0021274 256.7565 103.1364 16.45762372250012
| Epoch (UTC): | 16 May 2023 18:04:23 |
| Eccentricity: | 0.0021274 |
| inclination: | 97.3113° |
| perigee height: | 136 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 234.2974° |
| argument of perigee: | 256.7565° |
| revolutions per day: | 16.45762372 |
| mean anomaly at epoch: | 103.1364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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