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 67610U 26145.16286219 +.00000000 +00000-0 +11155-2 0 00001
2 67610 97.2833 214.8690 0001248 44.7209 315.4157 15.75205013 00
| Epoch (UTC): | 25 May 2026 03:54:31 |
| Eccentricity: | 0.0001248 |
| inclination: | 97.2833° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 214.8690° |
| argument of perigee: | 44.7209° |
| revolutions per day: | 15.75205013 |
| mean anomaly at epoch: | 315.4157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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