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 27846U 03031G 23272.47308983 .00000479 00000-0 23305-3 0 9998
2 27846 98.6895 277.4118 0009840 152.1099 208.0608 14.22794845 50603
| Epoch (UTC): | 29 September 2023 11:21:14 |
| Eccentricity: | 0.0009840 |
| inclination: | 98.6895° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 277.4118° |
| argument of perigee: | 152.1099° |
| revolutions per day: | 14.22794845 |
| mean anomaly at epoch: | 208.0608° |
| orbit number at epoch: | 5060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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