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 115U 60002D 25133.38408957 .00003544 00000-0 34071-3 0 9997
2 115 48.1631 262.8069 0028516 260.3214 99.4482 14.94889707479413
| Epoch (UTC): | 13 May 2025 09:13:05 |
| Eccentricity: | 0.0028516 |
| inclination: | 48.1631° |
| perigee height: | 563 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 262.8069° |
| argument of perigee: | 260.3214° |
| revolutions per day: | 14.94889707 |
| mean anomaly at epoch: | 99.4482° |
| orbit number at epoch: | 47941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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