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 62406U 26145.59023038 +.00000000 +00000-0 +34619-3 0 00005
2 62406 97.6277 101.3696 0017693 56.2020 304.0890 15.08588124 01
| Epoch (UTC): | 25 May 2026 14:09:55 |
| Eccentricity: | 0.0017693 |
| inclination: | 97.6277° |
| perigee height: | 528 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 101.3696° |
| argument of perigee: | 56.2020° |
| revolutions per day: | 15.08588124 |
| mean anomaly at epoch: | 304.0890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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