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 26067.98199810 +.00000000 +00000-0 +92348-4 0 00004
2 23343 97.7110 98.8283 0005725 213.1569 209.1432 14.79407254 00
| Epoch (UTC): | 08 March 2026 23:34:04 |
| Eccentricity: | 0.0005725 |
| inclination: | 97.7110° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 98.8283° |
| argument of perigee: | 213.1569° |
| revolutions per day: | 14.79407254 |
| mean anomaly at epoch: | 209.1432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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