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 65629U 26145.45746918 +.00000000 +00000-0 +86592-3 0 00006
2 65629 53.1607 309.8610 0000806 93.0228 267.0867 15.34404447 09
| Epoch (UTC): | 25 May 2026 10:58:45 |
| Eccentricity: | 0.0000806 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.8610° |
| argument of perigee: | 93.0228° |
| revolutions per day: | 15.34404447 |
| mean anomaly at epoch: | 267.0867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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