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 65657U 26145.40411819 +.00000000 +00000-0 +38465-3 0 00007
2 65657 97.4476 189.2866 0000477 158.4861 201.6387 15.05659282 09
| Epoch (UTC): | 25 May 2026 09:41:55 |
| Eccentricity: | 0.0000477 |
| inclination: | 97.4476° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 189.2866° |
| argument of perigee: | 158.4861° |
| revolutions per day: | 15.05659282 |
| mean anomaly at epoch: | 201.6387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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