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 26109.18708642 +.00000000 +00000-0 +15545-3 0 00004
2 23405 70.9816 267.2871 0000841 148.2804 211.8370 14.15569151 00
| Epoch (UTC): | 19 April 2026 04:29:24 |
| Eccentricity: | 0.0000841 |
| inclination: | 70.9816° |
| perigee height: | 840 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 267.2871° |
| argument of perigee: | 148.2804° |
| revolutions per day: | 14.15569151 |
| mean anomaly at epoch: | 211.8370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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