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 65188U 26145.59717294 +.00000000 +00000-0 +14607-3 0 00004
2 65188 97.4526 18.0917 0002385 65.0483 295.0992 15.05656078 02
| Epoch (UTC): | 25 May 2026 14:19:55 |
| Eccentricity: | 0.0002385 |
| inclination: | 97.4526° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0917° |
| argument of perigee: | 65.0483° |
| revolutions per day: | 15.05656078 |
| mean anomaly at epoch: | 295.0992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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