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 59U 60013B 25189.05952110 .00000086 00000-0 -37092-5 0 9993
2 59 28.2496 91.7603 0188912 306.6105 51.7199 13.53140175197394
| Epoch (UTC): | 08 July 2025 01:25:42 |
| Eccentricity: | 0.0188912 |
| inclination: | 28.2496° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 91.7603° |
| argument of perigee: | 306.6105° |
| revolutions per day: | 13.53140175 |
| mean anomaly at epoch: | 51.7199° |
| orbit number at epoch: | 19739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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