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 56329U 26144.95256273 +.00000000 +00000-0 -12786-3 0 00002
2 56329 97.4488 146.0485 0001933 92.5195 267.6253 15.05665883 00
| Epoch (UTC): | 24 May 2026 22:51:41 |
| Eccentricity: | 0.0001933 |
| inclination: | 97.4488° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.0485° |
| argument of perigee: | 92.5195° |
| revolutions per day: | 15.05665883 |
| mean anomaly at epoch: | 267.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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