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 23342U 26042.00665719 +.00000000 +00000-0 +10791-3 0 00006
2 23342 97.6734 65.2143 0002032 103.3411 256.8030 14.84890832 04
| Epoch (UTC): | 11 February 2026 00:09:35 |
| Eccentricity: | 0.0002032 |
| inclination: | 97.6734° |
| perigee height: | 613 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 65.2143° |
| argument of perigee: | 103.3411° |
| revolutions per day: | 14.84890832 |
| mean anomaly at epoch: | 256.8030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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