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 64948U 26145.40551727 +.00000000 +00000-0 +46604-3 0 00006
2 64948 97.4493 9.3865 0002734 90.9624 269.1917 15.05659045 01
| Epoch (UTC): | 25 May 2026 09:43:56 |
| Eccentricity: | 0.0002734 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.3865° |
| argument of perigee: | 90.9624° |
| revolutions per day: | 15.05659045 |
| mean anomaly at epoch: | 269.1917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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