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 18986U 26072.74012596 +.00000000 +00000-0 +11781-3 0 00007
2 18986 82.9580 188.5989 0040394 255.6943 103.9728 13.78933558 00
| Epoch (UTC): | 13 March 2026 17:45:46 |
| Eccentricity: | 0.0040394 |
| inclination: | 82.9580° |
| perigee height: | 938 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 188.5989° |
| argument of perigee: | 255.6943° |
| revolutions per day: | 13.78933558 |
| mean anomaly at epoch: | 103.9728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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