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 67735U 26145.59430566 +.00000000 +00000-0 +84629-3 0 00009
2 67735 97.2860 199.1395 0000461 226.6956 133.4248 15.33456288 06
| Epoch (UTC): | 25 May 2026 14:15:48 |
| Eccentricity: | 0.0000461 |
| inclination: | 97.2860° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1395° |
| argument of perigee: | 226.6956° |
| revolutions per day: | 15.33456288 |
| mean anomaly at epoch: | 133.4248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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