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 58U 60013A 25312.60824838 .00000132 00000-0 67472-4 0 9991
2 58 28.3258 178.9796 0164913 181.2994 178.7132 13.46419817204311
| Epoch (UTC): | 08 November 2025 14:35:52 |
| Eccentricity: | 0.0164913 |
| inclination: | 28.3258° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 178.9796° |
| argument of perigee: | 181.2994° |
| revolutions per day: | 13.46419817 |
| mean anomaly at epoch: | 178.7132° |
| orbit number at epoch: | 20431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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