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 25194.12748569 .00000049 00000-0 29783-4 0 9996
2 27386 98.3350 148.9658 0001364 84.9642 286.4661 14.38926836224791
| Epoch (UTC): | 13 July 2025 03:03:34 |
| Eccentricity: | 0.0001364 |
| inclination: | 98.3350° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 148.9658° |
| argument of perigee: | 84.9642° |
| revolutions per day: | 14.38926836 |
| mean anomaly at epoch: | 286.4661° |
| orbit number at epoch: | 22479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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