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 60740U 26145.07428779 +.00000000 +00000-0 -28856-4 0 00006
2 60740 53.1610 273.7709 0000948 115.4690 244.6409 15.30194831 01
| Epoch (UTC): | 25 May 2026 01:46:58 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.1610° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 273.7709° |
| argument of perigee: | 115.4690° |
| revolutions per day: | 15.30194831 |
| mean anomaly at epoch: | 244.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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