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 68803U 26145.12179405 +.00000000 +00000-0 +13677-2 0 00001
2 68803 97.2845 351.7507 0003369 60.3123 299.8477 15.75185411 00
| Epoch (UTC): | 25 May 2026 02:55:23 |
| Eccentricity: | 0.0003369 |
| inclination: | 97.2845° |
| perigee height: | 342 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 351.7507° |
| argument of perigee: | 60.3123° |
| revolutions per day: | 15.75185411 |
| mean anomaly at epoch: | 299.8477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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