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 25341.01488350 .00005747 00000-0 51584-3 0 9998
2 00115 48.1632 325.3310 0026577 111.9922 248.3824 14.96628677489336
| Epoch (UTC): | 07 December 2025 00:21:25 |
| Eccentricity: | 0.0026577 |
| inclination: | 48.1632° |
| perigee height: | 559 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 325.3310° |
| argument of perigee: | 111.9922° |
| revolutions per day: | 14.96628677 |
| mean anomaly at epoch: | 248.3824° |
| orbit number at epoch: | 48933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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