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 65231U 26145.59447194 +.00000000 +00000-0 +11359-3 0 00003
2 65231 86.5019 21.1823 0001682 87.7968 272.3359 13.24411666 02
| Epoch (UTC): | 25 May 2026 14:16:02 |
| Eccentricity: | 0.0001682 |
| inclination: | 86.5019° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1823° |
| argument of perigee: | 87.7968° |
| revolutions per day: | 13.24411666 |
| mean anomaly at epoch: | 272.3359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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