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 65660U 26145.12997219 +.00000000 +00000-0 -80354-4 0 00009
2 65660 97.4441 189.0394 0002097 121.7295 238.4137 15.05659594 00
| Epoch (UTC): | 25 May 2026 03:07:09 |
| Eccentricity: | 0.0002097 |
| inclination: | 97.4441° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.0394° |
| argument of perigee: | 121.7295° |
| revolutions per day: | 15.05659594 |
| mean anomaly at epoch: | 238.4137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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