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 64534U 26145.27682191 +.00000000 +00000-0 +14396-3 0 00005
2 64534 97.4732 260.3695 0003896 241.7071 118.3771 15.19951415 04
| Epoch (UTC): | 25 May 2026 06:38:37 |
| Eccentricity: | 0.0003896 |
| inclination: | 97.4732° |
| perigee height: | 503 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 260.3695° |
| argument of perigee: | 241.7071° |
| revolutions per day: | 15.19951415 |
| mean anomaly at epoch: | 118.3771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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