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 52468U 26145.09132593 +.00000000 +00000-0 -55781-4 0 00009
2 52468 53.2147 76.1383 0001698 88.1259 271.9928 15.08843685 00
| Epoch (UTC): | 25 May 2026 02:11:30 |
| Eccentricity: | 0.0001698 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 76.1383° |
| argument of perigee: | 88.1259° |
| revolutions per day: | 15.08843685 |
| mean anomaly at epoch: | 271.9928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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