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 64451U 26145.07274697 +.00000000 +00000-0 +74305-3 0 00005
2 64451 53.1574 94.0257 0001188 105.4822 254.6310 15.30221147 01
| Epoch (UTC): | 25 May 2026 01:44:45 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.0257° |
| argument of perigee: | 105.4822° |
| revolutions per day: | 15.30221147 |
| mean anomaly at epoch: | 254.6310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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