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 60198U 26145.21839145 +.00000000 +00000-0 +39003-5 0 00008
2 60198 53.1615 326.9510 0001068 97.3348 262.7775 15.31699027 01
| Epoch (UTC): | 25 May 2026 05:14:29 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 326.9510° |
| argument of perigee: | 97.3348° |
| revolutions per day: | 15.31699027 |
| mean anomaly at epoch: | 262.7775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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