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 25396U 26138.70364148 +.00000000 +00000-0 +44566-4 0 00000
2 25396 98.9857 129.0579 0001661 234.4448 125.6576 14.25751241 03
| Epoch (UTC): | 18 May 2026 16:53:14 |
| Eccentricity: | 0.0001661 |
| inclination: | 98.9857° |
| perigee height: | 805 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 129.0579° |
| argument of perigee: | 234.4448° |
| revolutions per day: | 14.25751241 |
| mean anomaly at epoch: | 125.6576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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