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 65678U 26145.59285786 +.00000000 +00000-0 +57640-3 0 00008
2 65678 53.1597 348.7646 0001252 97.7950 262.3193 15.30208616 07
| Epoch (UTC): | 25 May 2026 14:13:42 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.7646° |
| argument of perigee: | 97.7950° |
| revolutions per day: | 15.30208616 |
| mean anomaly at epoch: | 262.3193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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