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 60452U 26145.46241485 +.00000000 +00000-0 +14495-3 0 00008
2 60452 44.9997 152.4146 0007555 22.9136 337.2078 15.15837928 08
| Epoch (UTC): | 25 May 2026 11:05:52 |
| Eccentricity: | 0.0007555 |
| inclination: | 44.9997° |
| perigee height: | 513 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 152.4146° |
| argument of perigee: | 22.9136° |
| revolutions per day: | 15.15837928 |
| mean anomaly at epoch: | 337.2078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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