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 62816U 26144.88377494 +.00000000 +00000-0 +20196-3 0 00004
2 62816 53.1604 315.7135 0001125 87.4056 272.7073 15.30193908 05
| Epoch (UTC): | 24 May 2026 21:12:38 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 315.7135° |
| argument of perigee: | 87.4056° |
| revolutions per day: | 15.30193908 |
| mean anomaly at epoch: | 272.7073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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