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 23405U 26137.59398433 +.00000000 +00000-0 +13839-3 0 00007
2 23405 70.9824 207.5249 0001190 6.1263 353.9874 14.15570252 05
| Epoch (UTC): | 17 May 2026 14:15:20 |
| Eccentricity: | 0.0001190 |
| inclination: | 70.9824° |
| perigee height: | 840 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 207.5249° |
| argument of perigee: | 6.1263° |
| revolutions per day: | 14.15570252 |
| mean anomaly at epoch: | 353.9874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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