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 41340U 26145.56536627 +.00000000 +00000-0 +91093-3 0 00008
2 41340 30.9873 243.3220 0003230 126.5506 233.5450 15.81929841 03
| Epoch (UTC): | 25 May 2026 13:34:07 |
| Eccentricity: | 0.0003230 |
| inclination: | 30.9873° |
| perigee height: | 323 km |
| apogee height: | 327 km |
| right ascension of ascending node: | 243.3220° |
| argument of perigee: | 126.5506° |
| revolutions per day: | 15.81929841 |
| mean anomaly at epoch: | 233.5450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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