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 57392U 26145.30201602 +.00000000 +00000-0 +19833-4 0 00009
2 57392 99.5608 269.8394 0019081 75.9491 284.3774 13.68419993 08
| Epoch (UTC): | 25 May 2026 07:14:54 |
| Eccentricity: | 0.0019081 |
| inclination: | 99.5608° |
| perigee height: | 991 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 269.8394° |
| argument of perigee: | 75.9491° |
| revolutions per day: | 13.68419993 |
| mean anomaly at epoch: | 284.3774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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