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 25170.39502090 .00000118 00000-0 38247-4 0 9995
2 00059 28.2458 187.6633 0189004 149.9094 211.2460 13.53139631193999
| Epoch (UTC): | 19 June 2025 09:28:49 |
| Eccentricity: | 0.0189004 |
| inclination: | 28.2458° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 187.6633° |
| argument of perigee: | 149.9094° |
| revolutions per day: | 13.53139631 |
| mean anomaly at epoch: | 211.2460° |
| orbit number at epoch: | 19399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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