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 66371U 26145.53719147 +.00000000 +00000-0 +29110-3 0 00007
2 66371 53.1579 233.1689 0001068 80.2599 279.8522 15.30199723 00
| Epoch (UTC): | 25 May 2026 12:53:33 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1689° |
| argument of perigee: | 80.2599° |
| revolutions per day: | 15.30199723 |
| mean anomaly at epoch: | 279.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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