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 26071.99307426 +.00000000 +00000-0 +11666-3 0 00006
2 23342 97.6710 94.0908 0001956 75.9195 284.2238 14.84949666 09
| Epoch (UTC): | 12 March 2026 23:50:01 |
| Eccentricity: | 0.0001956 |
| inclination: | 97.6710° |
| perigee height: | 612 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 94.0908° |
| argument of perigee: | 75.9195° |
| revolutions per day: | 14.84949666 |
| mean anomaly at epoch: | 284.2238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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