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 16881U 86055A 25339.09336720 .00033349 00000-0 69061-3 0 9997
2 16881 82.4914 207.0407 0007264 145.6669 214.5050 15.45577135128977
| Epoch (UTC): | 05 December 2025 02:14:26 |
| Eccentricity: | 0.0007264 |
| inclination: | 82.4914° |
| perigee height: | 425 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 207.0407° |
| argument of perigee: | 145.6669° |
| revolutions per day: | 15.45577135 |
| mean anomaly at epoch: | 214.5050° |
| orbit number at epoch: | 12897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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