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 66546U 26145.75205632 +.00000000 +00000-0 +43799-3 0 00003
2 66546 51.7969 284.4662 0009005 176.0735 184.0314 15.15352551 05
| Epoch (UTC): | 25 May 2026 18:02:57 |
| Eccentricity: | 0.0009005 |
| inclination: | 51.7969° |
| perigee height: | 514 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 284.4662° |
| argument of perigee: | 176.0735° |
| revolutions per day: | 15.15352551 |
| mean anomaly at epoch: | 184.0314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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