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 05094U 71015U 25321.76787294 .00027514 00000-0 38869-2 0 9990
2 05094 65.6849 87.7604 0360251 268.4468 87.5342 14.41227821658566
| Epoch (UTC): | 17 November 2025 18:25:44 |
| Eccentricity: | 0.0360251 |
| inclination: | 65.6849° |
| perigee height: | 497 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 87.7604° |
| argument of perigee: | 268.4468° |
| revolutions per day: | 14.41227821 |
| mean anomaly at epoch: | 87.5342° |
| orbit number at epoch: | 65856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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