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 39151U 13018B 25118.76632518 .00006405 00000-0 65959-3 0 9999
2 39151 98.0671 246.7027 0014767 89.1811 271.1098 14.90547646648904
| Epoch (UTC): | 28 April 2025 18:23:30 |
| Eccentricity: | 0.0014767 |
| inclination: | 98.0671° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 246.7027° |
| argument of perigee: | 89.1811° |
| revolutions per day: | 14.90547646 |
| mean anomaly at epoch: | 271.1098° |
| orbit number at epoch: | 64890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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