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 00058U 60013A 23035.88363244 .00000125 00000-0 62056-4 0 9995
2 00058 28.3256 251.9222 0164866 117.4147 244.3271 13.46344230 68401
| Epoch (UTC): | 04 February 2023 21:12:25 |
| Eccentricity: | 0.0164866 |
| inclination: | 28.3256° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 251.9222° |
| argument of perigee: | 117.4147° |
| revolutions per day: | 13.46344230 |
| mean anomaly at epoch: | 244.3271° |
| orbit number at epoch: | 6840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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