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 25260U 26150.26817241 +.00000000 +00000-0 +10989-3 0 00003
2 25260 98.2456 246.1813 0011223 278.6451 81.3475 14.56088930 00
| Epoch (UTC): | 30 May 2026 06:26:10 |
| Eccentricity: | 0.0011223 |
| inclination: | 98.2456° |
| perigee height: | 698 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 246.1813° |
| argument of perigee: | 278.6451° |
| revolutions per day: | 14.56088930 |
| mean anomaly at epoch: | 81.3475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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