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 66995U 26145.17759153 +.00000000 +00000-0 +28615-3 0 00009
2 66995 97.6308 221.1410 0016253 78.3283 281.9766 15.06362011 03
| Epoch (UTC): | 25 May 2026 04:15:43 |
| Eccentricity: | 0.0016253 |
| inclination: | 97.6308° |
| perigee height: | 536 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 221.1410° |
| argument of perigee: | 78.3283° |
| revolutions per day: | 15.06362011 |
| mean anomaly at epoch: | 281.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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