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 26160.05971480 +.00000000 +00000-0 +69275-4 0 00009
2 23342 97.6626 178.8576 0002199 96.1893 263.9573 14.85076025 04
| Epoch (UTC): | 09 June 2026 01:25:59 |
| Eccentricity: | 0.0002199 |
| inclination: | 97.6626° |
| perigee height: | 612 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 178.8576° |
| argument of perigee: | 96.1893° |
| revolutions per day: | 14.85076025 |
| mean anomaly at epoch: | 263.9573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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