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 56232U 26145.33636404 +.00000000 +00000-0 +38733-3 0 00005
2 56232 49.9919 103.9129 0005628 92.4421 267.7191 15.53593501 09
| Epoch (UTC): | 25 May 2026 08:04:21 |
| Eccentricity: | 0.0005628 |
| inclination: | 49.9919° |
| perigee height: | 402 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 103.9129° |
| argument of perigee: | 92.4421° |
| revolutions per day: | 15.53593501 |
| mean anomaly at epoch: | 267.7191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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