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 27386U 02009A 25200.47430462 .00000066 00000-0 35326-4 0 9991
2 27386 98.3355 155.1344 0001331 83.4605 26.3184 14.38928323225701
| Epoch (UTC): | 19 July 2025 11:22:59 |
| Eccentricity: | 0.0001331 |
| inclination: | 98.3355° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 155.1344° |
| argument of perigee: | 83.4605° |
| revolutions per day: | 14.38928323 |
| mean anomaly at epoch: | 26.3184° |
| orbit number at epoch: | 22570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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