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 26106.71384441 +.00000000 +00000-0 +12441-3 0 00009
2 23405 70.9812 272.4910 0000995 156.2249 203.8920 14.15567715 06
| Epoch (UTC): | 16 April 2026 17:07:56 |
| Eccentricity: | 0.0000995 |
| inclination: | 70.9812° |
| perigee height: | 840 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 272.4910° |
| argument of perigee: | 156.2249° |
| revolutions per day: | 14.15567715 |
| mean anomaly at epoch: | 203.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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