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 27601U 02056E 23151.96317038 .00000302 00000-0 12345-3 0 9991
2 27601 98.1915 144.0643 0070590 302.2859 110.9866 14.32366602 69068
| Epoch (UTC): | 31 May 2023 23:06:57 |
| Eccentricity: | 0.0070590 |
| inclination: | 98.1915° |
| perigee height: | 733 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 144.0643° |
| argument of perigee: | 302.2859° |
| revolutions per day: | 14.32366602 |
| mean anomaly at epoch: | 110.9866° |
| orbit number at epoch: | 6906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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