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 40302U 14070E 24304.92016278 .14555910 24222-5 75248-3 0 9995
2 40302 97.0699 313.9580 0008498 243.4054 116.6377 16.42023614554487
| Epoch (UTC): | 30 October 2024 22:05:02 |
| Eccentricity: | 0.0008498 |
| inclination: | 97.0699° |
| perigee height: | 155 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 313.9580° |
| argument of perigee: | 243.4054° |
| revolutions per day: | 16.42023614 |
| mean anomaly at epoch: | 116.6377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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