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 64781U 26145.55146913 +.00000000 +00000-0 +69154-3 0 00009
2 64781 53.1596 244.7367 0001786 91.3040 268.8167 15.34416874 00
| Epoch (UTC): | 25 May 2026 13:14:06 |
| Eccentricity: | 0.0001786 |
| inclination: | 53.1596° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 244.7367° |
| argument of perigee: | 91.3040° |
| revolutions per day: | 15.34416874 |
| mean anomaly at epoch: | 268.8167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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