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 65852U 26145.73829830 +.00000000 +00000-0 +17563-3 0 00002
2 65852 34.9981 36.6576 0003720 285.3005 74.7289 14.91744820 07
| Epoch (UTC): | 25 May 2026 17:43:08 |
| Eccentricity: | 0.0003720 |
| inclination: | 34.9981° |
| perigee height: | 590 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 36.6576° |
| argument of perigee: | 285.3005° |
| revolutions per day: | 14.91744820 |
| mean anomaly at epoch: | 74.7289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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