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 65656U 26145.07736944 +.00000000 +00000-0 -10356-3 0 00008
2 65656 97.4493 188.9596 0001377 121.0725 239.0637 15.05640955 08
| Epoch (UTC): | 25 May 2026 01:51:24 |
| Eccentricity: | 0.0001377 |
| inclination: | 97.4493° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.9596° |
| argument of perigee: | 121.0725° |
| revolutions per day: | 15.05640955 |
| mean anomaly at epoch: | 239.0637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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