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 25316.90839277 .00000129 00000-0 61420-4 0 9994
2 00058 28.3258 157.1594 0164915 216.9106 141.9989 13.46420265204893
| Epoch (UTC): | 12 November 2025 21:48:05 |
| Eccentricity: | 0.0164915 |
| inclination: | 28.3258° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 157.1594° |
| argument of perigee: | 216.9106° |
| revolutions per day: | 13.46420265 |
| mean anomaly at epoch: | 141.9989° |
| orbit number at epoch: | 20489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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