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 25140.53572182 .00002778 00000-0 27170-3 0 9994
2 115 48.1623 227.8017 0028535 291.7621 68.0260 14.94941225480488
| Epoch (UTC): | 20 May 2025 12:51:26 |
| Eccentricity: | 0.0028535 |
| inclination: | 48.1623° |
| perigee height: | 562 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 227.8017° |
| argument of perigee: | 291.7621° |
| revolutions per day: | 14.94941225 |
| mean anomaly at epoch: | 68.0260° |
| orbit number at epoch: | 48048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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