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 37152U 10043A 23274.18691090 .00000031 00000-0 15481-3 0 9994
2 37152 82.4579 324.2921 0002568 124.9455 289.9703 12.42932347592561
| Epoch (UTC): | 01 October 2023 04:29:09 |
| Eccentricity: | 0.0002568 |
| inclination: | 82.4579° |
| perigee height: | 1492 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 324.2921° |
| argument of perigee: | 124.9455° |
| revolutions per day: | 12.42932347 |
| mean anomaly at epoch: | 289.9703° |
| orbit number at epoch: | 59256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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