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 65613U 26145.45162750 +.00000000 +00000-0 +35538-3 0 00009
2 65613 97.4511 213.9834 0002653 130.6138 229.5320 15.05659108 01
| Epoch (UTC): | 25 May 2026 10:50:20 |
| Eccentricity: | 0.0002653 |
| inclination: | 97.4511° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9834° |
| argument of perigee: | 130.6138° |
| revolutions per day: | 15.05659108 |
| mean anomaly at epoch: | 229.5320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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