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 25349.99337220 .00000208 00000-0 21898-3 0 9990
2 00082 38.8570 320.2218 1166966 59.2184 311.8184 12.27813119 54285
| Epoch (UTC): | 15 December 2025 23:50:27 |
| Eccentricity: | 0.1166966 |
| inclination: | 38.8570° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 320.2218° |
| argument of perigee: | 59.2184° |
| revolutions per day: | 12.27813119 |
| mean anomaly at epoch: | 311.8184° |
| orbit number at epoch: | 5428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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