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 23343U 26106.82529398 +.00000000 +00000-0 +38972-4 0 00002
2 23343 97.7052 136.0886 0008119 96.3414 76.7600 14.79449659 09
| Epoch (UTC): | 16 April 2026 19:48:25 |
| Eccentricity: | 0.0008119 |
| inclination: | 97.7052° |
| perigee height: | 625 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 136.0886° |
| argument of perigee: | 96.3414° |
| revolutions per day: | 14.79449659 |
| mean anomaly at epoch: | 76.7600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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