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 20453U 26022.53082910 +.00000000 +00000-0 +94577-3 0 00002
2 20453 35.6056 116.3177 0100743 191.4690 168.3744 15.49562385 03
| Epoch (UTC): | 22 January 2026 12:44:23 |
| Eccentricity: | 0.0100743 |
| inclination: | 35.6056° |
| perigee height: | 350 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 116.3177° |
| argument of perigee: | 191.4690° |
| revolutions per day: | 15.49562385 |
| mean anomaly at epoch: | 168.3744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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