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 40538U 15015A 25267.90151365 0.00000000 00000-0 00000-0 0 07
2 40538 97.3733 338.1672 0005659 1.1922 358.8077 15.27648914 09
| Epoch (UTC): | 24 September 2025 21:38:10 |
| Eccentricity: | 0.0005659 |
| inclination: | 97.3733° |
| perigee height: | 479 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 338.1672° |
| argument of perigee: | 1.1922° |
| revolutions per day: | 15.27648914 |
| mean anomaly at epoch: | 358.8077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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