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 65628U 26144.84809813 +.00000000 +00000-0 +80141-3 0 00005
2 65628 53.1601 312.4612 0000481 165.9954 194.1062 15.34409743 09
| Epoch (UTC): | 24 May 2026 20:21:15 |
| Eccentricity: | 0.0000481 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 312.4612° |
| argument of perigee: | 165.9954° |
| revolutions per day: | 15.34409743 |
| mean anomaly at epoch: | 194.1062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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