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 66150U 26145.20642288 +.00000000 +00000-0 -15490-2 0 00003
2 66150 53.1564 67.3892 0005378 101.9803 258.1801 15.30129326 01
| Epoch (UTC): | 25 May 2026 04:57:14 |
| Eccentricity: | 0.0005378 |
| inclination: | 53.1564° |
| perigee height: | 472 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 67.3892° |
| argument of perigee: | 101.9803° |
| revolutions per day: | 15.30129326 |
| mean anomaly at epoch: | 258.1801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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