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 65624U 26145.16892522 +.00000000 +00000-0 +64397-3 0 00001
2 65624 53.1613 309.4762 0001263 97.3183 262.7967 15.42180993 09
| Epoch (UTC): | 25 May 2026 04:03:15 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.1613° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 309.4762° |
| argument of perigee: | 97.3183° |
| revolutions per day: | 15.42180993 |
| mean anomaly at epoch: | 262.7967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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