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 23028.93896186 .00000241 00000-0 25018-3 0 9992
2 00082 38.8521 260.6800 1167405 14.6130 348.5508 12.26086480925084
| Epoch (UTC): | 28 January 2023 22:32:06 |
| Eccentricity: | 0.1167405 |
| inclination: | 38.8521° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 260.6800° |
| argument of perigee: | 14.6130° |
| revolutions per day: | 12.26086480 |
| mean anomaly at epoch: | 348.5508° |
| orbit number at epoch: | 92508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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