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 68383U 26145.37924525 +.00000000 +00000-0 +38270-3 0 00009
2 68383 97.2848 287.8740 0000844 80.7100 279.4238 15.33449385 06
| Epoch (UTC): | 25 May 2026 09:06:06 |
| Eccentricity: | 0.0000844 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.8740° |
| argument of perigee: | 80.7100° |
| revolutions per day: | 15.33449385 |
| mean anomaly at epoch: | 279.4238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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