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 65861U 26145.13108205 +.00000000 +00000-0 +65002-3 0 00003
2 65861 53.1603 298.7940 0001475 79.2006 280.9163 15.34398996 02
| Epoch (UTC): | 25 May 2026 03:08:45 |
| Eccentricity: | 0.0001475 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 298.7940° |
| argument of perigee: | 79.2006° |
| revolutions per day: | 15.34398996 |
| mean anomaly at epoch: | 280.9163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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