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 65116U 26145.34395356 +.00000000 +00000-0 +31772-3 0 00001
2 65116 42.0103 141.7595 0005887 58.5857 301.5544 15.00610520 01
| Epoch (UTC): | 25 May 2026 08:15:17 |
| Eccentricity: | 0.0005887 |
| inclination: | 42.0103° |
| perigee height: | 561 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 141.7595° |
| argument of perigee: | 58.5857° |
| revolutions per day: | 15.00610520 |
| mean anomaly at epoch: | 301.5544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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