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 00085U 61004C 25125.94948765 .00651259 00000-0 10175-1 0 9994
2 00085 38.6286 339.3938 0047379 217.4608 142.2872 15.49493407188429
| Epoch (UTC): | 05 May 2025 22:47:15 |
| Eccentricity: | 0.0047379 |
| inclination: | 38.6286° |
| perigee height: | 386 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 339.3938° |
| argument of perigee: | 217.4608° |
| revolutions per day: | 15.49493407 |
| mean anomaly at epoch: | 142.2872° |
| orbit number at epoch: | 18842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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