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 40021U 14033M 23087.89499920 .00012396 00000-0 10936-2 0 9990
2 40021 98.0500 49.3950 0011577 169.7812 190.3646 14.96505186477176
| Epoch (UTC): | 28 March 2023 21:28:47 |
| Eccentricity: | 0.0011577 |
| inclination: | 98.0500° |
| perigee height: | 569 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 49.3950° |
| argument of perigee: | 169.7812° |
| revolutions per day: | 14.96505186 |
| mean anomaly at epoch: | 190.3646° |
| orbit number at epoch: | 47717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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