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 64528U 26145.58613227 +.00000000 +00000-0 +32590-3 0 00002
2 64528 97.4605 260.9308 0003601 257.4623 102.6211 15.23649115 05
| Epoch (UTC): | 25 May 2026 14:04:01 |
| Eccentricity: | 0.0003601 |
| inclination: | 97.4605° |
| perigee height: | 492 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 260.9308° |
| argument of perigee: | 257.4623° |
| revolutions per day: | 15.23649115 |
| mean anomaly at epoch: | 102.6211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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