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 66706U 26145.15479846 +.00000000 +00000-0 +27119-3 0 00003
2 66706 97.4246 219.1856 0005577 87.7408 272.4465 15.19635545 03
| Epoch (UTC): | 25 May 2026 03:42:54 |
| Eccentricity: | 0.0005577 |
| inclination: | 97.4246° |
| perigee height: | 503 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.1856° |
| argument of perigee: | 87.7408° |
| revolutions per day: | 15.19635545 |
| mean anomaly at epoch: | 272.4465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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