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 64960U 26145.56023772 +.00000000 +00000-0 +84411-4 0 00000
2 64960 86.4920 290.0396 0001869 94.9025 265.2322 13.24406162 09
| Epoch (UTC): | 25 May 2026 13:26:44 |
| Eccentricity: | 0.0001869 |
| inclination: | 86.4920° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.0396° |
| argument of perigee: | 94.9025° |
| revolutions per day: | 13.24406162 |
| mean anomaly at epoch: | 265.2322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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