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 43259U 26145.59533207 +.00000000 +00000-0 +11973-3 0 00002
2 43259 98.0534 208.1841 0004661 85.1235 275.0506 14.76443246 05
| Epoch (UTC): | 25 May 2026 14:17:16 |
| Eccentricity: | 0.0004661 |
| inclination: | 98.0534° |
| perigee height: | 637 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 208.1841° |
| argument of perigee: | 85.1235° |
| revolutions per day: | 14.76443246 |
| mean anomaly at epoch: | 275.0506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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