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 65428U 26145.51775721 +.00000000 +00000-0 +87876-3 0 00000
2 65428 53.1592 235.7175 0001818 88.0630 272.0579 15.30216932 09
| Epoch (UTC): | 25 May 2026 12:25:34 |
| Eccentricity: | 0.0001818 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.7175° |
| argument of perigee: | 88.0630° |
| revolutions per day: | 15.30216932 |
| mean anomaly at epoch: | 272.0579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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