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 25188.73221542 .00000170 00000-0 18108-3 0 9990
2 00082 38.8535 199.0592 1167156 358.7316 1.0517 12.27665501 34465
| Epoch (UTC): | 07 July 2025 17:34:23 |
| Eccentricity: | 0.1167156 |
| inclination: | 38.8535° |
| perigee height: | 633 km |
| apogee height: | 2486 km |
| right ascension of ascending node: | 199.0592° |
| argument of perigee: | 358.7316° |
| revolutions per day: | 12.27665501 |
| mean anomaly at epoch: | 1.0517° |
| orbit number at epoch: | 3446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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