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 64254U 26145.63761957 +.00000000 +00000-0 +71220-3 0 00001
2 64254 43.0018 232.8234 0001549 261.2525 98.8152 15.27594438 06
| Epoch (UTC): | 25 May 2026 15:18:10 |
| Eccentricity: | 0.0001549 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.8234° |
| argument of perigee: | 261.2525° |
| revolutions per day: | 15.27594438 |
| mean anomaly at epoch: | 98.8152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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