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 64936U 26145.58273404 +.00000000 +00000-0 +10674-2 0 00002
2 64936 97.4507 9.4531 0000882 63.7917 296.3401 15.05684280 09
| Epoch (UTC): | 25 May 2026 13:59:08 |
| Eccentricity: | 0.0000882 |
| inclination: | 97.4507° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 9.4531° |
| argument of perigee: | 63.7917° |
| revolutions per day: | 15.05684280 |
| mean anomaly at epoch: | 296.3401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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