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 17912U 87038B 25187.99373619 .00000335 00000-0 36416-4 0 9991
2 17912 82.5014 168.1724 0017806 255.3880 104.5362 14.85054926 42768
| Epoch (UTC): | 06 July 2025 23:50:58 |
| Eccentricity: | 0.0017806 |
| inclination: | 82.5014° |
| perigee height: | 601 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 168.1724° |
| argument of perigee: | 255.3880° |
| revolutions per day: | 14.85054926 |
| mean anomaly at epoch: | 104.5362° |
| orbit number at epoch: | 4276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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