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 23464U 26100.18597442 +.00000000 +00000-0 +13023-3 0 00003
2 23464 82.9254 68.9526 0040537 339.9466 20.0094 13.73071127 03
| Epoch (UTC): | 10 April 2026 04:27:48 |
| Eccentricity: | 0.0040537 |
| inclination: | 82.9254° |
| perigee height: | 959 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 68.9526° |
| argument of perigee: | 339.9466° |
| revolutions per day: | 13.73071127 |
| mean anomaly at epoch: | 20.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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