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 22148.48813563 .00000120 00000-0 42125-4 0 9990
2 00059 28.2459 170.8657 0189279 125.7526 236.0779 13.53000262 42477
| Epoch (UTC): | 28 May 2022 11:42:54 |
| Eccentricity: | 0.0189279 |
| inclination: | 28.2459° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 170.8657° |
| argument of perigee: | 125.7526° |
| revolutions per day: | 13.53000262 |
| mean anomaly at epoch: | 236.0779° |
| orbit number at epoch: | 4247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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