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 37792U 11044E 25134.18167374 .00000980 00000-0 13450-3 0 9993
2 37792 98.2325 51.8132 0052683 205.5518 154.3088 14.79902014739891
| Epoch (UTC): | 14 May 2025 04:21:36 |
| Eccentricity: | 0.0052683 |
| inclination: | 98.2325° |
| perigee height: | 593 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 51.8132° |
| argument of perigee: | 205.5518° |
| revolutions per day: | 14.79902014 |
| mean anomaly at epoch: | 154.3088° |
| orbit number at epoch: | 73989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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