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 23038.71733520 .00000254 00000-0 26627-3 0 9992
2 00082 38.8498 224.4751 1167148 61.8285 309.5337 12.26092504926283
| Epoch (UTC): | 07 February 2023 17:12:57 |
| Eccentricity: | 0.1167148 |
| inclination: | 38.8498° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 224.4751° |
| argument of perigee: | 61.8285° |
| revolutions per day: | 12.26092504 |
| mean anomaly at epoch: | 309.5337° |
| orbit number at epoch: | 92628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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