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 23030.48726227 .00000216 00000-0 23063-3 0 9993
2 00082 38.8515 254.9474 1167351 22.0871 342.6163 12.26087261925276
| Epoch (UTC): | 30 January 2023 11:41:39 |
| Eccentricity: | 0.1167351 |
| inclination: | 38.8515° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 254.9474° |
| argument of perigee: | 22.0871° |
| revolutions per day: | 12.26087261 |
| mean anomaly at epoch: | 342.6163° |
| orbit number at epoch: | 92527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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