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 66816U 26145.12562382 +.00000000 +00000-0 +18002-2 0 00000
2 66816 43.0024 42.2894 0001990 298.0802 61.9848 15.27627271 05
| Epoch (UTC): | 25 May 2026 03:00:53 |
| Eccentricity: | 0.0001990 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 42.2894° |
| argument of perigee: | 298.0802° |
| revolutions per day: | 15.27627271 |
| mean anomaly at epoch: | 61.9848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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