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 56749U 26145.59551191 +.00000000 +00000-0 +51489-3 0 00008
2 56749 97.4933 352.5705 0005181 75.3773 284.8052 15.49134739 07
| Epoch (UTC): | 25 May 2026 14:17:32 |
| Eccentricity: | 0.0005181 |
| inclination: | 97.4933° |
| perigee height: | 416 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 352.5705° |
| argument of perigee: | 75.3773° |
| revolutions per day: | 15.49134739 |
| mean anomaly at epoch: | 284.8052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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