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 23343.62376005 .00000273 00000-0 28193-3 0 9993
2 00082 38.8494 175.5067 1163998 93.7756 279.6496 12.26444281963716
| Epoch (UTC): | 09 December 2023 14:58:12 |
| Eccentricity: | 0.1163998 |
| inclination: | 38.8494° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 175.5067° |
| argument of perigee: | 93.7756° |
| revolutions per day: | 12.26444281 |
| mean anomaly at epoch: | 279.6496° |
| orbit number at epoch: | 96371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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