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 39440U 13066AA 25114.80316922 .00009651 00000-0 98270-3 0 9990
2 39440 97.8467 59.7010 0061780 332.9207 26.8792 14.89507160615820
| Epoch (UTC): | 24 April 2025 19:16:33 |
| Eccentricity: | 0.0061780 |
| inclination: | 97.8467° |
| perigee height: | 556 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 59.7010° |
| argument of perigee: | 332.9207° |
| revolutions per day: | 14.89507160 |
| mean anomaly at epoch: | 26.8792° |
| orbit number at epoch: | 61582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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