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 60506U 26145.48311451 +.00000000 +00000-0 +23873-3 0 00001
2 60506 97.3738 224.4812 0004873 45.0305 315.1330 15.29760136 04
| Epoch (UTC): | 25 May 2026 11:35:41 |
| Eccentricity: | 0.0004873 |
| inclination: | 97.3738° |
| perigee height: | 473 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 224.4812° |
| argument of perigee: | 45.0305° |
| revolutions per day: | 15.29760136 |
| mean anomaly at epoch: | 315.1330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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