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 03892U 69037C 24262.75057590 .00000045 00000-0 15697-3 0 9991
2 03892 99.9195 172.4763 0039068 171.5633 247.2688 13.42075090714064
| Epoch (UTC): | 18 September 2024 18:00:49 |
| Eccentricity: | 0.0039068 |
| inclination: | 99.9195° |
| perigee height: | 1072 km |
| apogee height: | 1131 km |
| right ascension of ascending node: | 172.4763° |
| argument of perigee: | 171.5633° |
| revolutions per day: | 13.42075090 |
| mean anomaly at epoch: | 247.2688° |
| orbit number at epoch: | 71406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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