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 is defined by the following mean orbital elements,
1 25732U 26128.13832095 +.00000000 +00000-0 +33371-4 0 00003
2 25732 98.6517 170.9782 0037313 172.1570 253.0634 14.18276471 05
| Epoch (UTC): | 08 May 2026 03:19:10 |
| Eccentricity: | 0.0037313 |
| inclination: | 98.6517° |
| perigee height: | 804 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 170.9782° |
| argument of perigee: | 172.1570° |
| revolutions per day: | 14.18276471 |
| mean anomaly at epoch: | 253.0634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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