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 60435U 26145.38009041 +.00000000 +00000-0 +37850-4 0 00001
2 60435 53.1606 220.0030 0000645 76.8618 283.2457 15.34390915 00
| Epoch (UTC): | 25 May 2026 09:07:19 |
| Eccentricity: | 0.0000645 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 220.0030° |
| argument of perigee: | 76.8618° |
| revolutions per day: | 15.34390915 |
| mean anomaly at epoch: | 283.2457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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