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 40057U 26129.84281478 +.00000000 +00000-0 +34035-3 0 00009
2 40057 98.2561 32.6780 0008563 43.2338 316.9553 14.97528138 00
| Epoch (UTC): | 09 May 2026 20:13:39 |
| Eccentricity: | 0.0008563 |
| inclination: | 98.2561° |
| perigee height: | 569 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 32.6780° |
| argument of perigee: | 43.2338° |
| revolutions per day: | 14.97528138 |
| mean anomaly at epoch: | 316.9553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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