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 66872U 26145.64202499 +.00000000 +00000-0 +63572-3 0 00002
2 66872 43.0043 268.9456 0000174 328.2133 31.8708 15.27592601 04
| Epoch (UTC): | 25 May 2026 15:24:30 |
| Eccentricity: | 0.0000174 |
| inclination: | 43.0043° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 268.9456° |
| argument of perigee: | 328.2133° |
| revolutions per day: | 15.27592601 |
| mean anomaly at epoch: | 31.8708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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