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 65283U 26145.16380137 +.00000000 +00000-0 +74800-4 0 00007
2 65283 97.4502 197.6054 0001255 148.9471 211.1831 15.05651616 05
| Epoch (UTC): | 25 May 2026 03:55:52 |
| Eccentricity: | 0.0001255 |
| inclination: | 97.4502° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 197.6054° |
| argument of perigee: | 148.9471° |
| revolutions per day: | 15.05651616 |
| mean anomaly at epoch: | 211.1831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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