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 67695U 26145.57474721 +.00000000 +00000-0 +66074-3 0 00007
2 67695 97.2853 257.1547 0000191 222.5813 137.5415 15.33441768 02
| Epoch (UTC): | 25 May 2026 13:47:38 |
| Eccentricity: | 0.0000191 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1547° |
| argument of perigee: | 222.5813° |
| revolutions per day: | 15.33441768 |
| mean anomaly at epoch: | 137.5415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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