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 60514U 26145.15948184 +.00000000 +00000-0 +39065-3 0 00003
2 60514 97.3790 229.2212 0003137 52.6416 307.5115 15.40009754 08
| Epoch (UTC): | 25 May 2026 03:49:39 |
| Eccentricity: | 0.0003137 |
| inclination: | 97.3790° |
| perigee height: | 444 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 229.2212° |
| argument of perigee: | 52.6416° |
| revolutions per day: | 15.40009754 |
| mean anomaly at epoch: | 307.5115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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