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 18313U 26020.14365449 +.00000000 +00000-0 +37749-4 0 00009
2 18313 82.5552 59.3727 0011100 125.1322 235.0881 13.84300186 08
| Epoch (UTC): | 20 January 2026 03:26:51 |
| Eccentricity: | 0.0011100 |
| inclination: | 82.5552° |
| perigee height: | 941 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 59.3727° |
| argument of perigee: | 125.1322° |
| revolutions per day: | 13.84300186 |
| mean anomaly at epoch: | 235.0881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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