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 23087U 94023A 23152.39525800 .00000165 00000-0 11161-3 0 9998
2 23087 71.0530 132.2976 0007390 145.9468 214.2130 14.13965603501696
| Epoch (UTC): | 01 June 2023 09:29:10 |
| Eccentricity: | 0.0007390 |
| inclination: | 71.0530° |
| perigee height: | 840 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 132.2976° |
| argument of perigee: | 145.9468° |
| revolutions per day: | 14.13965603 |
| mean anomaly at epoch: | 214.2130° |
| orbit number at epoch: | 50169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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