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 24357.59809972 .00017521 00000-0 57726-3 0 9994
2 16881 82.4965 202.4997 0011378 340.9003 19.1809 15.31285752 75551
| Epoch (UTC): | 22 December 2024 14:21:15 |
| Eccentricity: | 0.0011378 |
| inclination: | 82.4965° |
| perigee height: | 464 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 202.4997° |
| argument of perigee: | 340.9003° |
| revolutions per day: | 15.31285752 |
| mean anomaly at epoch: | 19.1809° |
| orbit number at epoch: | 7555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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