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 27387U 02009B 25144.58536804 .00000068 00000-0 38697-4 0 9994
2 27387 98.8158 148.4751 0031890 191.0949 168.9537 14.36674480217543
| Epoch (UTC): | 24 May 2025 14:02:55 |
| Eccentricity: | 0.0031890 |
| inclination: | 98.8158° |
| perigee height: | 747 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 148.4751° |
| argument of perigee: | 191.0949° |
| revolutions per day: | 14.36674480 |
| mean anomaly at epoch: | 168.9537° |
| orbit number at epoch: | 21754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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