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 18693U 26071.78166948 +.00000000 +00000-0 -41040-2 0 00007
2 18693 101.7135 17.1847 0209567 312.0552 62.8558 12.98084460 08
| Epoch (UTC): | 12 March 2026 18:45:36 |
| Eccentricity: | 0.0209567 |
| inclination: | 101.7135° |
| perigee height: | 1109 km |
| apogee height: | 1430 km |
| right ascension of ascending node: | 17.1847° |
| argument of perigee: | 312.0552° |
| revolutions per day: | 12.98084460 |
| mean anomaly at epoch: | 62.8558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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