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 68165U 26145.31795226 +.00000000 +00000-0 +57811-3 0 00007
2 68165 97.2856 167.0185 0001891 93.8378 266.3081 15.33453073 00
| Epoch (UTC): | 25 May 2026 07:37:51 |
| Eccentricity: | 0.0001891 |
| inclination: | 97.2856° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 167.0185° |
| argument of perigee: | 93.8378° |
| revolutions per day: | 15.33453073 |
| mean anomaly at epoch: | 266.3081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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