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 27387U 02009B 23027.55259910 .00000167 00000-0 72602-4 0 9993
2 27387 98.7435 3.4506 0032390 174.9369 185.2150 14.36130388 95776
| Epoch (UTC): | 27 January 2023 13:15:44 |
| Eccentricity: | 0.0032390 |
| inclination: | 98.7435° |
| perigee height: | 748 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 3.4506° |
| argument of perigee: | 174.9369° |
| revolutions per day: | 14.36130388 |
| mean anomaly at epoch: | 185.2150° |
| orbit number at epoch: | 9577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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