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 65899U 26145.06288608 +.00000000 +00000-0 +97897-3 0 00009
2 65899 53.1596 15.4414 0000594 49.8212 310.2842 15.34410571 02
| Epoch (UTC): | 25 May 2026 01:30:33 |
| Eccentricity: | 0.0000594 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 15.4414° |
| argument of perigee: | 49.8212° |
| revolutions per day: | 15.34410571 |
| mean anomaly at epoch: | 310.2842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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