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 65296U 26145.42686441 +.00000000 +00000-0 +26352-3 0 00005
2 65296 97.4502 197.8677 0000380 197.6913 162.4301 15.05654770 06
| Epoch (UTC): | 25 May 2026 10:14:41 |
| Eccentricity: | 0.0000380 |
| inclination: | 97.4502° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 197.8677° |
| argument of perigee: | 197.6913° |
| revolutions per day: | 15.05654770 |
| mean anomaly at epoch: | 162.4301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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