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 00082U 61004B 23263.88221015 .00000553 00000-0 52240-3 0 9993
2 00082 38.8512 110.8225 1163815 68.7281 303.3567 12.26307900953920
| Epoch (UTC): | 20 September 2023 21:10:22 |
| Eccentricity: | 0.1163815 |
| inclination: | 38.8512° |
| perigee height: | 641 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 110.8225° |
| argument of perigee: | 68.7281° |
| revolutions per day: | 12.26307900 |
| mean anomaly at epoch: | 303.3567° |
| orbit number at epoch: | 95392 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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