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 25137.84932723 .00000122 00000-0 53131-4 0 9991
2 00058 28.3296 345.7124 0164889 174.2339 186.0143 13.46410843180743
| Epoch (UTC): | 17 May 2025 20:23:01 |
| Eccentricity: | 0.0164889 |
| inclination: | 28.3296° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 345.7124° |
| argument of perigee: | 174.2339° |
| revolutions per day: | 13.46410843 |
| mean anomaly at epoch: | 186.0143° |
| orbit number at epoch: | 18074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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