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 25137.39248081 .00000586 00000-0 52212-3 0 9998
2 00082 38.8569 29.6627 1166654 110.3559 262.6171 12.27631790 28155
| Epoch (UTC): | 17 May 2025 09:25:10 |
| Eccentricity: | 0.1166654 |
| inclination: | 38.8569° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 29.6627° |
| argument of perigee: | 110.3559° |
| revolutions per day: | 12.27631790 |
| mean anomaly at epoch: | 262.6171° |
| orbit number at epoch: | 2815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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