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 23038.55288663 .00000126 00000-0 60841-4 0 9994
2 00058 28.3253 238.3791 0164885 139.5178 221.7761 13.46344486 68763
| Epoch (UTC): | 07 February 2023 13:16:09 |
| Eccentricity: | 0.0164885 |
| inclination: | 28.3253° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 238.3791° |
| argument of perigee: | 139.5178° |
| revolutions per day: | 13.46344486 |
| mean anomaly at epoch: | 221.7761° |
| orbit number at epoch: | 6876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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