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 42015U 17008BV 23332.13550576 .11791653 24087-5 42855-3 0 9999
2 42015 97.1503 39.8233 0008517 270.0130 90.0196 16.43624330378556
| Epoch (UTC): | 28 November 2023 03:15:07 |
| Eccentricity: | 0.0008517 |
| inclination: | 97.1503° |
| perigee height: | 150 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 39.8233° |
| argument of perigee: | 270.0130° |
| revolutions per day: | 16.43624330 |
| mean anomaly at epoch: | 90.0196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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