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 60433U 26145.59877110 +.00000000 +00000-0 +27599-4 0 00001
2 60433 53.1603 219.9439 0001181 80.7519 279.3616 15.30186510 08
| Epoch (UTC): | 25 May 2026 14:22:13 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 219.9439° |
| argument of perigee: | 80.7519° |
| revolutions per day: | 15.30186510 |
| mean anomaly at epoch: | 279.3616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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