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 64834U 26145.45638875 +.00000000 +00000-0 +22774-3 0 00007
2 64834 51.9003 306.1319 0000629 101.1763 258.9270 14.79936372 08
| Epoch (UTC): | 25 May 2026 10:57:11 |
| Eccentricity: | 0.0000629 |
| inclination: | 51.9003° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 306.1319° |
| argument of perigee: | 101.1763° |
| revolutions per day: | 14.79936372 |
| mean anomaly at epoch: | 258.9270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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