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 18958U 26040.70626453 +.00000000 +00000-0 +17756-3 0 00008
2 18958 82.5121 278.5986 0003120 315.8966 44.2019 15.17741890 04
| Epoch (UTC): | 09 February 2026 16:57:01 |
| Eccentricity: | 0.0003120 |
| inclination: | 82.5121° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 278.5986° |
| argument of perigee: | 315.8966° |
| revolutions per day: | 15.17741890 |
| mean anomaly at epoch: | 44.2019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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