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 64090U 26145.65033176 +.00000000 +00000-0 +23976-3 0 00001
2 64090 97.4693 221.5485 0013893 85.4415 274.8406 15.18566045 09
| Epoch (UTC): | 25 May 2026 15:36:28 |
| Eccentricity: | 0.0013893 |
| inclination: | 97.4693° |
| perigee height: | 501 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 221.5485° |
| argument of perigee: | 85.4415° |
| revolutions per day: | 15.18566045 |
| mean anomaly at epoch: | 274.8406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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