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 116U 61015A 25338.44541383 .00000075 00000-0 11581-3 0 9995
2 116 66.8106 7.3400 0070171 46.0717 314.6124 13.92285972269592
| Epoch (UTC): | 04 December 2025 10:41:23 |
| Eccentricity: | 0.0070171 |
| inclination: | 66.8106° |
| perigee height: | 869 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 7.3400° |
| argument of perigee: | 46.0717° |
| revolutions per day: | 13.92285972 |
| mean anomaly at epoch: | 314.6124° |
| orbit number at epoch: | 26959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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