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 25197.67443386 .00002373 00000-0 23361-3 0 9993
2 00115 48.1637 308.0303 0027754 190.8080 169.2244 14.95265102467871
| Epoch (UTC): | 16 July 2025 16:11:11 |
| Eccentricity: | 0.0027754 |
| inclination: | 48.1637° |
| perigee height: | 562 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 308.0303° |
| argument of perigee: | 190.8080° |
| revolutions per day: | 14.95265102 |
| mean anomaly at epoch: | 169.2244° |
| orbit number at epoch: | 46787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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