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 66725U 26145.47086741 +.00000000 +00000-0 +30355-3 0 00003
2 66725 97.4177 219.3603 0004337 105.8904 254.2809 15.19848643 00
| Epoch (UTC): | 25 May 2026 11:18:02 |
| Eccentricity: | 0.0004337 |
| inclination: | 97.4177° |
| perigee height: | 503 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.3603° |
| argument of perigee: | 105.8904° |
| revolutions per day: | 15.19848643 |
| mean anomaly at epoch: | 254.2809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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