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 66724U 26145.18159286 +.00000000 +00000-0 +27507-3 0 00000
2 66724 97.4187 219.3158 0003262 54.4394 305.7145 15.20465350 00
| Epoch (UTC): | 25 May 2026 04:21:29 |
| Eccentricity: | 0.0003262 |
| inclination: | 97.4187° |
| perigee height: | 502 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.3158° |
| argument of perigee: | 54.4394° |
| revolutions per day: | 15.20465350 |
| mean anomaly at epoch: | 305.7145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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