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 66544U 26145.43857866 +.00000000 +00000-0 +75851-3 0 00002
2 66544 42.9989 204.2793 0000592 266.4517 93.6267 15.27595134 07
| Epoch (UTC): | 25 May 2026 10:31:33 |
| Eccentricity: | 0.0000592 |
| inclination: | 42.9989° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 204.2793° |
| argument of perigee: | 266.4517° |
| revolutions per day: | 15.27595134 |
| mean anomaly at epoch: | 93.6267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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