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 25348.26531372 .00000131 00000-0 52699-4 0 9995
2 00059 28.2507 353.7220 0188879 203.2325 155.9586 13.53155007218101
| Epoch (UTC): | 14 December 2025 06:22:03 |
| Eccentricity: | 0.0188879 |
| inclination: | 28.2507° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 353.7220° |
| argument of perigee: | 203.2325° |
| revolutions per day: | 13.53155007 |
| mean anomaly at epoch: | 155.9586° |
| orbit number at epoch: | 21810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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