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 43440U 26145.59186257 +.00000000 +00000-0 +28124-3 0 00009
2 43440 97.0405 164.1661 0003314 15.3690 344.7649 15.24671796 07
| Epoch (UTC): | 25 May 2026 14:12:16 |
| Eccentricity: | 0.0003314 |
| inclination: | 97.0405° |
| perigee height: | 489 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 164.1661° |
| argument of perigee: | 15.3690° |
| revolutions per day: | 15.24671796 |
| mean anomaly at epoch: | 344.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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