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 65518U 26145.34267084 +.00000000 +00000-0 +64637-3 0 00009
2 65518 53.1609 274.4010 0000499 95.3711 264.7349 15.34402872 08
| Epoch (UTC): | 25 May 2026 08:13:26 |
| Eccentricity: | 0.0000499 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 274.4010° |
| argument of perigee: | 95.3711° |
| revolutions per day: | 15.34402872 |
| mean anomaly at epoch: | 264.7349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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