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 25188.97795171 .00009798 00000-0 25187-3 0 9997
2 16881 82.4936 1.4499 0008650 353.3581 6.7548 15.39083549127043
| Epoch (UTC): | 07 July 2025 23:28:15 |
| Eccentricity: | 0.0008650 |
| inclination: | 82.4936° |
| perigee height: | 443 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 1.4499° |
| argument of perigee: | 353.3581° |
| revolutions per day: | 15.39083549 |
| mean anomaly at epoch: | 6.7548° |
| orbit number at epoch: | 12704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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