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 64770U 26145.55356919 +.00000000 +00000-0 +66789-3 0 00007
2 64770 53.1590 244.7575 0001873 28.1623 331.9481 15.34397152 03
| Epoch (UTC): | 25 May 2026 13:17:08 |
| Eccentricity: | 0.0001873 |
| inclination: | 53.1590° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 244.7575° |
| argument of perigee: | 28.1623° |
| revolutions per day: | 15.34397152 |
| mean anomaly at epoch: | 331.9481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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