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 64909U 26144.85329182 +.00000000 +00000-0 +66061-3 0 00008
2 64909 53.1599 351.9718 0000979 85.4183 274.6930 15.30211942 09
| Epoch (UTC): | 24 May 2026 20:28:44 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1599° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.9718° |
| argument of perigee: | 85.4183° |
| revolutions per day: | 15.30211942 |
| mean anomaly at epoch: | 274.6930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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