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 39152U 13018C 23083.29767805 .00017541 00000-0 21431-2 0 9994
2 39152 97.8502 171.1269 0016534 43.1681 317.0825 14.83234158535291
| Epoch (UTC): | 24 March 2023 07:08:39 |
| Eccentricity: | 0.0016534 |
| inclination: | 97.8502° |
| perigee height: | 607 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 171.1269° |
| argument of perigee: | 43.1681° |
| revolutions per day: | 14.83234158 |
| mean anomaly at epoch: | 317.0825° |
| orbit number at epoch: | 53529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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