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 00059U 60013B 25193.85515024 .00000096 00000-0 12108-4 0 9995
2 00059 28.2499 67.1201 0188872 346.8723 12.6957 13.53140275197170
| Epoch (UTC): | 12 July 2025 20:31:24 |
| Eccentricity: | 0.0188872 |
| inclination: | 28.2499° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 67.1201° |
| argument of perigee: | 346.8723° |
| revolutions per day: | 13.53140275 |
| mean anomaly at epoch: | 12.6957° |
| orbit number at epoch: | 19717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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