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 56336U 26145.44134176 +.00000000 +00000-0 -62930-6 0 00001
2 56336 97.4476 145.3993 0001454 94.4965 265.6429 15.05650535 06
| Epoch (UTC): | 25 May 2026 10:35:31 |
| Eccentricity: | 0.0001454 |
| inclination: | 97.4476° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3993° |
| argument of perigee: | 94.4965° |
| revolutions per day: | 15.05650535 |
| mean anomaly at epoch: | 265.6429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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