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 25321.85416910 .00000123 00000-0 47732-4 0 9994
2 00059 28.2470 129.4299 0188999 341.5221 17.8534 13.53153225214529
| Epoch (UTC): | 17 November 2025 20:30:00 |
| Eccentricity: | 0.0188999 |
| inclination: | 28.2470° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 129.4299° |
| argument of perigee: | 341.5221° |
| revolutions per day: | 13.53153225 |
| mean anomaly at epoch: | 17.8534° |
| orbit number at epoch: | 21452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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