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 65895U 26145.34657703 +.00000000 +00000-0 +87163-3 0 00007
2 65895 53.1603 14.3716 0001511 91.4957 268.6218 15.34413242 00
| Epoch (UTC): | 25 May 2026 08:19:04 |
| Eccentricity: | 0.0001511 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.3716° |
| argument of perigee: | 91.4957° |
| revolutions per day: | 15.34413242 |
| mean anomaly at epoch: | 268.6218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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