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 67809U 26145.46109372 +.00000000 +00000-0 +68768-3 0 00001
2 67809 97.2861 333.5128 0002245 82.7160 277.4338 15.33453594 03
| Epoch (UTC): | 25 May 2026 11:03:58 |
| Eccentricity: | 0.0002245 |
| inclination: | 97.2861° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5128° |
| argument of perigee: | 82.7160° |
| revolutions per day: | 15.33453594 |
| mean anomaly at epoch: | 277.4338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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