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 66743U 26145.45489602 +.00000000 +00000-0 +25542-3 0 00006
2 66743 97.4195 219.4356 0003420 91.1316 269.0311 15.19998116 05
| Epoch (UTC): | 25 May 2026 10:55:03 |
| Eccentricity: | 0.0003420 |
| inclination: | 97.4195° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.4356° |
| argument of perigee: | 91.1316° |
| revolutions per day: | 15.19998116 |
| mean anomaly at epoch: | 269.0311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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