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 64049U 26145.65652359 +.00000000 +00000-0 +13444-3 0 00004
2 64049 97.3801 218.0218 0000446 224.7333 135.3866 15.19765778 01
| Epoch (UTC): | 25 May 2026 15:45:23 |
| Eccentricity: | 0.0000446 |
| inclination: | 97.3801° |
| perigee height: | 506 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 218.0218° |
| argument of perigee: | 224.7333° |
| revolutions per day: | 15.19765778 |
| mean anomaly at epoch: | 135.3866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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