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 25171.72289204 .00000116 00000-0 34844-4 0 9999
2 00059 28.2460 180.8396 0188984 161.0606 199.7081 13.53139666194171
| Epoch (UTC): | 20 June 2025 17:20:57 |
| Eccentricity: | 0.0188984 |
| inclination: | 28.2460° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 180.8396° |
| argument of perigee: | 161.0606° |
| revolutions per day: | 13.53139666 |
| mean anomaly at epoch: | 199.7081° |
| orbit number at epoch: | 19417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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