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 25199.50977124 .00011787 00000-0 30096-3 0 9994
2 16881 82.4951 350.6606 0007857 311.3091 48.7477 15.39310632107464
| Epoch (UTC): | 18 July 2025 12:14:04 |
| Eccentricity: | 0.0007857 |
| inclination: | 82.4951° |
| perigee height: | 443 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 350.6606° |
| argument of perigee: | 311.3091° |
| revolutions per day: | 15.39310632 |
| mean anomaly at epoch: | 48.7477° |
| orbit number at epoch: | 10746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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