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 27940U 03042B 25339.91887094 .00001525 00000-0 26777-3 0 9994
2 27940 98.3721 147.8936 0012030 243.9557 116.0409 14.69171205186184
| Epoch (UTC): | 05 December 2025 22:03:10 |
| Eccentricity: | 0.0012030 |
| inclination: | 98.3721° |
| perigee height: | 655 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 147.8936° |
| argument of perigee: | 243.9557° |
| revolutions per day: | 14.69171205 |
| mean anomaly at epoch: | 116.0409° |
| orbit number at epoch: | 18618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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