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 64725U 26145.39752363 +.00000000 +00000-0 +36064-3 0 00005
2 64725 53.1581 184.9275 0001130 88.3072 271.8059 15.30208404 07
| Epoch (UTC): | 25 May 2026 09:32:26 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9275° |
| argument of perigee: | 88.3072° |
| revolutions per day: | 15.30208404 |
| mean anomaly at epoch: | 271.8059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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