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 25140.51545095 .00000126 00000-0 46036-4 0 9992
2 00059 28.2514 341.1898 0189036 259.0862 98.8360 13.53137957189940
| Epoch (UTC): | 20 May 2025 12:22:14 |
| Eccentricity: | 0.0189036 |
| inclination: | 28.2514° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 341.1898° |
| argument of perigee: | 259.0862° |
| revolutions per day: | 13.53137957 |
| mean anomaly at epoch: | 98.8360° |
| orbit number at epoch: | 18994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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