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 66737U 26145.14971368 +.00000000 +00000-0 +28709-3 0 00008
2 66737 97.4240 219.3329 0003294 55.8247 304.3300 15.20171386 02
| Epoch (UTC): | 25 May 2026 03:35:35 |
| Eccentricity: | 0.0003294 |
| inclination: | 97.4240° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.3329° |
| argument of perigee: | 55.8247° |
| revolutions per day: | 15.20171386 |
| mean anomaly at epoch: | 304.3300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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