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 65016U 26144.81310399 +.00000000 +00000-0 +63541-3 0 00004
2 65016 53.1595 300.6927 0000802 97.1319 262.9773 15.30201536 07
| Epoch (UTC): | 24 May 2026 19:30:52 |
| Eccentricity: | 0.0000802 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.6927° |
| argument of perigee: | 97.1319° |
| revolutions per day: | 15.30201536 |
| mean anomaly at epoch: | 262.9773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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