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 64550U 26145.56769764 +.00000000 +00000-0 +21466-3 0 00003
2 64550 97.4600 260.7814 0001105 55.3194 304.8146 15.21784903 06
| Epoch (UTC): | 25 May 2026 13:37:29 |
| Eccentricity: | 0.0001105 |
| inclination: | 97.4600° |
| perigee height: | 500 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 260.7814° |
| argument of perigee: | 55.3194° |
| revolutions per day: | 15.21784903 |
| mean anomaly at epoch: | 304.8146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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