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 62330U 26145.60577563 +.00000000 +00000-0 +13842-3 0 00005
2 62330 86.5036 351.0155 0001309 92.4516 267.6768 13.24408627 03
| Epoch (UTC): | 25 May 2026 14:32:19 |
| Eccentricity: | 0.0001309 |
| inclination: | 86.5036° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 351.0155° |
| argument of perigee: | 92.4516° |
| revolutions per day: | 13.24408627 |
| mean anomaly at epoch: | 267.6768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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