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 62405U 26145.62539418 +.00000000 +00000-0 +84891-3 0 00009
2 62405 44.9768 6.4153 0008969 204.2116 155.8358 15.58272034 06
| Epoch (UTC): | 25 May 2026 15:00:34 |
| Eccentricity: | 0.0008969 |
| inclination: | 44.9768° |
| perigee height: | 387 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 6.4153° |
| argument of perigee: | 204.2116° |
| revolutions per day: | 15.58272034 |
| mean anomaly at epoch: | 155.8358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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