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 64836U 26145.45888674 +.00000000 +00000-0 +50807-3 0 00001
2 64836 51.9015 303.6305 0000564 102.3134 257.7891 14.79683257 00
| Epoch (UTC): | 25 May 2026 11:00:47 |
| Eccentricity: | 0.0000564 |
| inclination: | 51.9015° |
| perigee height: | 630 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 303.6305° |
| argument of perigee: | 102.3134° |
| revolutions per day: | 14.79683257 |
| mean anomaly at epoch: | 257.7891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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