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 62658U 26145.18840064 +.00000000 +00000-0 +33659-3 0 00008
2 62658 97.3890 227.1642 0002895 99.4099 260.7469 15.29658426 05
| Epoch (UTC): | 25 May 2026 04:31:17 |
| Eccentricity: | 0.0002895 |
| inclination: | 97.3890° |
| perigee height: | 475 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 227.1642° |
| argument of perigee: | 99.4099° |
| revolutions per day: | 15.29658426 |
| mean anomaly at epoch: | 260.7469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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