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 66660U 26145.08457641 +.00000000 +00000-0 +18840-3 0 00004
2 66660 97.7489 74.8522 0015660 94.9296 265.3712 14.93856372 09
| Epoch (UTC): | 25 May 2026 02:01:47 |
| Eccentricity: | 0.0015660 |
| inclination: | 97.7489° |
| perigee height: | 575 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 74.8522° |
| argument of perigee: | 94.9296° |
| revolutions per day: | 14.93856372 |
| mean anomaly at epoch: | 265.3712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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