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 64953U 26145.60765571 +.00000000 +00000-0 +42009-3 0 00003
2 64953 97.4521 9.5764 0002360 84.4379 275.7117 15.05665526 05
| Epoch (UTC): | 25 May 2026 14:35:01 |
| Eccentricity: | 0.0002360 |
| inclination: | 97.4521° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.5764° |
| argument of perigee: | 84.4379° |
| revolutions per day: | 15.05665526 |
| mean anomaly at epoch: | 275.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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