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 27848U 03031J 23267.51967149 .00000500 00000-0 24403-3 0 9999
2 27848 98.6843 273.7139 0009059 207.2663 152.8041 14.22380350 49620
| Epoch (UTC): | 24 September 2023 12:28:19 |
| Eccentricity: | 0.0009059 |
| inclination: | 98.6843° |
| perigee height: | 811 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 273.7139° |
| argument of perigee: | 207.2663° |
| revolutions per day: | 14.22380350 |
| mean anomaly at epoch: | 152.8041° |
| orbit number at epoch: | 4962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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