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 65904U 26145.65331729 +.00000000 +00000-0 +84196-3 0 00002
2 65904 53.1603 12.7302 0001538 110.0656 250.0512 15.34416816 09
| Epoch (UTC): | 25 May 2026 15:40:46 |
| Eccentricity: | 0.0001538 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 12.7302° |
| argument of perigee: | 110.0656° |
| revolutions per day: | 15.34416816 |
| mean anomaly at epoch: | 250.0512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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