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 25140.59253264 .00000122 00000-0 51984-4 0 9997
2 00058 28.3297 331.7940 0164894 196.9510 162.5475 13.46411005181113
| Epoch (UTC): | 20 May 2025 14:13:14 |
| Eccentricity: | 0.0164894 |
| inclination: | 28.3297° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 331.7940° |
| argument of perigee: | 196.9510° |
| revolutions per day: | 13.46411005 |
| mean anomaly at epoch: | 162.5475° |
| orbit number at epoch: | 18111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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