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 40143U 26145.60830741 +.00000000 +00000-0 +32091-3 0 00000
2 40143 97.1491 186.8179 0008740 160.2890 199.8689 15.25990033 07
| Epoch (UTC): | 25 May 2026 14:35:57 |
| Eccentricity: | 0.0008740 |
| inclination: | 97.1491° |
| perigee height: | 482 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 186.8179° |
| argument of perigee: | 160.2890° |
| revolutions per day: | 15.25990033 |
| mean anomaly at epoch: | 199.8689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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