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 62328U 26145.59812274 +.00000000 +00000-0 +15161-3 0 00007
2 62328 86.4982 350.7373 0001335 80.6218 279.5067 13.24405999 07
| Epoch (UTC): | 25 May 2026 14:21:17 |
| Eccentricity: | 0.0001335 |
| inclination: | 86.4982° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.7373° |
| argument of perigee: | 80.6218° |
| revolutions per day: | 13.24405999 |
| mean anomaly at epoch: | 279.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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