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 64853U 26145.31076442 +.00000000 +00000-0 +35275-3 0 00009
2 64853 97.4476 0.5998 0002339 86.9094 273.2400 15.05656932 09
| Epoch (UTC): | 25 May 2026 07:27:30 |
| Eccentricity: | 0.0002339 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.5998° |
| argument of perigee: | 86.9094° |
| revolutions per day: | 15.05656932 |
| mean anomaly at epoch: | 273.2400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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