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 46493U 26145.61695441 +.00000000 +00000-0 +33382-3 0 00005
2 46493 97.8749 153.2809 0009239 18.1210 342.0361 15.36750587 02
| Epoch (UTC): | 25 May 2026 14:48:24 |
| Eccentricity: | 0.0009239 |
| inclination: | 97.8749° |
| perigee height: | 449 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 153.2809° |
| argument of perigee: | 18.1210° |
| revolutions per day: | 15.36750587 |
| mean anomaly at epoch: | 342.0361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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