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 65764U 26145.48770396 +.00000000 +00000-0 +14125-2 0 00008
2 65764 51.9031 73.5465 0000903 93.4856 266.6210 14.79924148 08
| Epoch (UTC): | 25 May 2026 11:42:17 |
| Eccentricity: | 0.0000903 |
| inclination: | 51.9031° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 73.5465° |
| argument of perigee: | 93.4856° |
| revolutions per day: | 14.79924148 |
| mean anomaly at epoch: | 266.6210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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