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 65658U 26145.13275029 +.00000000 +00000-0 +34542-3 0 00001
2 65658 97.4490 189.0388 0000939 146.5773 213.5514 15.05654257 07
| Epoch (UTC): | 25 May 2026 03:11:09 |
| Eccentricity: | 0.0000939 |
| inclination: | 97.4490° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 189.0388° |
| argument of perigee: | 146.5773° |
| revolutions per day: | 15.05654257 |
| mean anomaly at epoch: | 213.5514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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