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 00115U 60002D 25313.10622358 .00006052 00000-0 54573-3 0 9996
2 00115 48.1616 102.2769 0027164 344.7384 15.2712 14.96344859485159
| Epoch (UTC): | 09 November 2025 02:32:57 |
| Eccentricity: | 0.0027164 |
| inclination: | 48.1616° |
| perigee height: | 559 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 102.2769° |
| argument of perigee: | 344.7384° |
| revolutions per day: | 14.96344859 |
| mean anomaly at epoch: | 15.2712° |
| orbit number at epoch: | 48515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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