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 23343U 26020.08556772 +.00000000 +00000-0 +91633-4 0 00004
2 23343 97.7166 52.8595 0007223 30.7539 342.8287 14.79339278 05
| Epoch (UTC): | 20 January 2026 02:03:13 |
| Eccentricity: | 0.0007223 |
| inclination: | 97.7166° |
| perigee height: | 626 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 52.8595° |
| argument of perigee: | 30.7539° |
| revolutions per day: | 14.79339278 |
| mean anomaly at epoch: | 342.8287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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