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 60468U 26145.10740773 +.00000000 +00000-0 +25008-3 0 00002
2 60468 97.3731 225.1163 0001836 325.3040 34.8081 15.32473099 08
| Epoch (UTC): | 25 May 2026 02:34:40 |
| Eccentricity: | 0.0001836 |
| inclination: | 97.3731° |
| perigee height: | 467 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 225.1163° |
| argument of perigee: | 325.3040° |
| revolutions per day: | 15.32473099 |
| mean anomaly at epoch: | 34.8081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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