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 62466U 26145.29739648 +.00000000 +00000-0 +14422-2 0 00008
2 62466 42.9988 120.8580 0001843 272.0067 88.0590 15.70904011 08
| Epoch (UTC): | 25 May 2026 07:08:15 |
| Eccentricity: | 0.0001843 |
| inclination: | 42.9988° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 120.8580° |
| argument of perigee: | 272.0067° |
| revolutions per day: | 15.70904011 |
| mean anomaly at epoch: | 88.0590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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