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 53384U 22096Q 24188.17644722 .15600392 26894-5 15301-3 0 9991
2 53384 97.3553 111.7586 0009951 211.7483 148.3223 16.50887592107457
| Epoch (UTC): | 06 July 2024 04:14:05 |
| Eccentricity: | 0.0009951 |
| inclination: | 97.3553° |
| perigee height: | 130 km |
| apogee height: | 143 km |
| right ascension of ascending node: | 111.7586° |
| argument of perigee: | 211.7483° |
| revolutions per day: | 16.50887592 |
| mean anomaly at epoch: | 148.3223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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