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 60486U 26145.15015203 +.00000000 +00000-0 +39265-3 0 00000
2 60486 97.3739 229.3164 0003025 18.8397 341.2962 15.41904264 00
| Epoch (UTC): | 25 May 2026 03:36:13 |
| Eccentricity: | 0.0003025 |
| inclination: | 97.3739° |
| perigee height: | 438 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 229.3164° |
| argument of perigee: | 18.8397° |
| revolutions per day: | 15.41904264 |
| mean anomaly at epoch: | 341.2962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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