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 26161.52177485 +.00000000 +00000-0 +18675-4 0 00005
2 18313 82.5575 307.2006 0011351 92.2769 267.9692 13.84307297 09
| Epoch (UTC): | 10 June 2026 12:31:21 |
| Eccentricity: | 0.0011351 |
| inclination: | 82.5575° |
| perigee height: | 940 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 307.2006° |
| argument of perigee: | 92.2769° |
| revolutions per day: | 13.84307297 |
| mean anomaly at epoch: | 267.9692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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