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 60512U 26145.50180343 +.00000000 +00000-0 +33171-3 0 00007
2 60512 97.3718 229.6888 0003595 12.9854 347.1484 15.41186859 04
| Epoch (UTC): | 25 May 2026 12:02:35 |
| Eccentricity: | 0.0003595 |
| inclination: | 97.3718° |
| perigee height: | 440 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 229.6888° |
| argument of perigee: | 12.9854° |
| revolutions per day: | 15.41186859 |
| mean anomaly at epoch: | 347.1484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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