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 25343.18647477 .00000048 00000-0 95052-4 0 9999
2 116 66.8103 355.7397 0070461 42.5180 318.1326 13.92287212270258
| Epoch (UTC): | 09 December 2025 04:28:31 |
| Eccentricity: | 0.0070461 |
| inclination: | 66.8103° |
| perigee height: | 869 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 355.7397° |
| argument of perigee: | 42.5180° |
| revolutions per day: | 13.92287212 |
| mean anomaly at epoch: | 318.1326° |
| orbit number at epoch: | 27025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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