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 64215U 26145.42605789 +.00000000 +00000-0 +45903-3 0 00004
2 64215 53.1595 43.2167 0001600 94.6509 265.4674 15.30206751 05
| Epoch (UTC): | 25 May 2026 10:13:31 |
| Eccentricity: | 0.0001600 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.2167° |
| argument of perigee: | 94.6509° |
| revolutions per day: | 15.30206751 |
| mean anomaly at epoch: | 265.4674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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