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 56744U 26145.62941190 +.00000000 +00000-0 +48837-3 0 00002
2 56744 97.5279 350.9338 0006580 58.7077 301.4813 15.41338872 03
| Epoch (UTC): | 25 May 2026 15:06:21 |
| Eccentricity: | 0.0006580 |
| inclination: | 97.5279° |
| perigee height: | 438 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 350.9338° |
| argument of perigee: | 58.7077° |
| revolutions per day: | 15.41338872 |
| mean anomaly at epoch: | 301.4813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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