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 65256U 26145.07601833 +.00000000 +00000-0 -23653-3 0 00006
2 65256 97.4505 187.9156 0000748 178.8995 181.2234 15.05641538 08
| Epoch (UTC): | 25 May 2026 01:49:27 |
| Eccentricity: | 0.0000748 |
| inclination: | 97.4505° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 187.9156° |
| argument of perigee: | 178.8995° |
| revolutions per day: | 15.05641538 |
| mean anomaly at epoch: | 181.2234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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