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 17304U 87006B 25193.90741473 .00000177 00000-0 65516-4 0 9993
2 17304 74.0576 69.8418 0030121 250.8014 108.9880 14.38955617 16751
| Epoch (UTC): | 12 July 2025 21:46:40 |
| Eccentricity: | 0.0030121 |
| inclination: | 74.0576° |
| perigee height: | 740 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 69.8418° |
| argument of perigee: | 250.8014° |
| revolutions per day: | 14.38955617 |
| mean anomaly at epoch: | 108.9880° |
| orbit number at epoch: | 1675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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