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 66481U 26145.53885854 +.00000000 +00000-0 +56923-3 0 00000
2 66481 43.0041 221.8022 0001508 261.3268 98.7413 15.27589863 04
| Epoch (UTC): | 25 May 2026 12:55:57 |
| Eccentricity: | 0.0001508 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.8022° |
| argument of perigee: | 261.3268° |
| revolutions per day: | 15.27589863 |
| mean anomaly at epoch: | 98.7413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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