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 62613U 26145.18714235 +.00000000 +00000-0 +37588-3 0 00004
2 62613 97.4005 227.2967 0004972 56.1308 304.0405 15.29232068 09
| Epoch (UTC): | 25 May 2026 04:29:29 |
| Eccentricity: | 0.0004972 |
| inclination: | 97.4005° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 227.2967° |
| argument of perigee: | 56.1308° |
| revolutions per day: | 15.29232068 |
| mean anomaly at epoch: | 304.0405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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