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 43585U 26145.64955266 +.00000000 +00000-0 +24653-3 0 00002
2 43585 97.1307 212.6025 0005282 69.5174 290.6647 15.54551636 06
| Epoch (UTC): | 25 May 2026 15:35:21 |
| Eccentricity: | 0.0005282 |
| inclination: | 97.1307° |
| perigee height: | 400 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 212.6025° |
| argument of perigee: | 69.5174° |
| revolutions per day: | 15.54551636 |
| mean anomaly at epoch: | 290.6647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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