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 64114U 26145.63524413 +.00000000 +00000-0 +18121-2 0 00000
2 64114 53.1594 29.3228 0001234 59.8431 300.2693 15.31717670 02
| Epoch (UTC): | 25 May 2026 15:14:45 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 29.3228° |
| argument of perigee: | 59.8431° |
| revolutions per day: | 15.31717670 |
| mean anomaly at epoch: | 300.2693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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