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 23026.08680561 .00000395 00000-0 37595-3 0 9997
2 00082 38.8536 271.2396 1167569 0.8402 359.3953 12.26084988924734
| Epoch (UTC): | 26 January 2023 02:05:00 |
| Eccentricity: | 0.1167569 |
| inclination: | 38.8536° |
| perigee height: | 638 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 271.2396° |
| argument of perigee: | 0.8402° |
| revolutions per day: | 12.26084988 |
| mean anomaly at epoch: | 359.3953° |
| orbit number at epoch: | 92473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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