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 43794U 26145.10663812 +.00000000 +00000-0 +24643-3 0 00007
2 43794 97.3981 197.1098 0032774 27.6289 332.6680 15.22516431 06
| Epoch (UTC): | 25 May 2026 02:33:33 |
| Eccentricity: | 0.0032774 |
| inclination: | 97.3981° |
| perigee height: | 476 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 197.1098° |
| argument of perigee: | 27.6289° |
| revolutions per day: | 15.22516431 |
| mean anomaly at epoch: | 332.6680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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