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 65536U 26145.60251027 +.00000000 +00000-0 +18694-3 0 00000
2 65536 97.4451 215.2282 0002251 147.6226 212.5140 15.05654036 07
| Epoch (UTC): | 25 May 2026 14:27:36 |
| Eccentricity: | 0.0002251 |
| inclination: | 97.4451° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.2282° |
| argument of perigee: | 147.6226° |
| revolutions per day: | 15.05654036 |
| mean anomaly at epoch: | 212.5140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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