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 18959U 26067.00742303 +.00000000 +00000-0 +78692-4 0 00001
2 18959 82.5398 171.2241 0017408 64.0096 296.2911 14.85673883 05
| Epoch (UTC): | 08 March 2026 00:10:41 |
| Eccentricity: | 0.0017408 |
| inclination: | 82.5398° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 171.2241° |
| argument of perigee: | 64.0096° |
| revolutions per day: | 14.85673883 |
| mean anomaly at epoch: | 296.2911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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