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 60495U 26145.22943124 +.00000000 +00000-0 +36291-3 0 00006
2 60495 97.3777 229.3943 0003372 32.6711 327.4744 15.40399404 03
| Epoch (UTC): | 25 May 2026 05:30:22 |
| Eccentricity: | 0.0003372 |
| inclination: | 97.3777° |
| perigee height: | 443 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 229.3943° |
| argument of perigee: | 32.6711° |
| revolutions per day: | 15.40399404 |
| mean anomaly at epoch: | 327.4744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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