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 25199.27814953 .00002443 00000-0 23974-3 0 9991
2 00115 48.1636 300.1760 0027789 197.8848 162.1093 14.95274812468117
| Epoch (UTC): | 18 July 2025 06:40:32 |
| Eccentricity: | 0.0027789 |
| inclination: | 48.1636° |
| perigee height: | 562 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 300.1760° |
| argument of perigee: | 197.8848° |
| revolutions per day: | 14.95274812 |
| mean anomaly at epoch: | 162.1093° |
| orbit number at epoch: | 46811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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