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 40381U 15004A 25256.86423495 0.00018500 00000-0 61058-3 0 07
2 40381 97.3768 319.4587 0009995 302.0190 57.9809 15.31397622 09
| Epoch (UTC): | 13 September 2025 20:44:29 |
| Eccentricity: | 0.0009995 |
| inclination: | 97.3768° |
| perigee height: | 465 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 319.4587° |
| argument of perigee: | 302.0190° |
| revolutions per day: | 15.31397622 |
| mean anomaly at epoch: | 57.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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