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 65056U 26145.20577002 +.00000000 +00000-0 +29275-3 0 00004
2 65056 97.4492 222.2760 0000929 130.2900 229.8408 15.05651552 03
| Epoch (UTC): | 25 May 2026 04:56:18 |
| Eccentricity: | 0.0000929 |
| inclination: | 97.4492° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 222.2760° |
| argument of perigee: | 130.2900° |
| revolutions per day: | 15.05651552 |
| mean anomaly at epoch: | 229.8408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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