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 27840U 03031A 23152.50551266 .00000158 00000-0 61961-4 0 9992
2 27840 98.4783 117.9900 0099059 63.4963 297.6342 14.39152834 46061
| Epoch (UTC): | 01 June 2023 12:07:56 |
| Eccentricity: | 0.0099059 |
| inclination: | 98.4783° |
| perigee height: | 690 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 117.9900° |
| argument of perigee: | 63.4963° |
| revolutions per day: | 14.39152834 |
| mean anomaly at epoch: | 297.6342° |
| orbit number at epoch: | 4606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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