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 25340.71691550 .00000468 00000-0 42254-3 0 9997
2 00082 38.8584 354.6761 1167218 14.2944 348.8024 12.27806249 53143
| Epoch (UTC): | 06 December 2025 17:12:21 |
| Eccentricity: | 0.1167218 |
| inclination: | 38.8584° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 354.6761° |
| argument of perigee: | 14.2944° |
| revolutions per day: | 12.27806249 |
| mean anomaly at epoch: | 348.8024° |
| orbit number at epoch: | 5314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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