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 25634U 26151.92131549 +.00000000 +00000-0 +54262-4 0 00005
2 25634 98.5117 118.6150 0011337 87.6039 272.6436 14.19985906 05
| Epoch (UTC): | 31 May 2026 22:06:41 |
| Eccentricity: | 0.0011337 |
| inclination: | 98.5117° |
| perigee height: | 817 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 118.6150° |
| argument of perigee: | 87.6039° |
| revolutions per day: | 14.19985906 |
| mean anomaly at epoch: | 272.6436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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