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 64572U 26145.55868573 +.00000000 +00000-0 +13765-3 0 00007
2 64572 97.7720 260.0610 0003115 67.1229 293.0319 14.93463308 08
| Epoch (UTC): | 25 May 2026 13:24:30 |
| Eccentricity: | 0.0003115 |
| inclination: | 97.7720° |
| perigee height: | 585 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 260.0610° |
| argument of perigee: | 67.1229° |
| revolutions per day: | 14.93463308 |
| mean anomaly at epoch: | 293.0319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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