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 65860U 26145.15212088 +.00000000 +00000-0 +69503-3 0 00009
2 65860 53.1607 298.9288 0001163 65.8929 294.2195 15.34399050 06
| Epoch (UTC): | 25 May 2026 03:39:03 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 298.9288° |
| argument of perigee: | 65.8929° |
| revolutions per day: | 15.34399050 |
| mean anomaly at epoch: | 294.2195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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