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 37853U 11061D 24280.44779109 .17770245 53761-5 25050-3 0 9997
2 37853 101.6502 153.3227 0006588 329.6103 30.4802 16.48847764709386
| Epoch (UTC): | 06 October 2024 10:44:49 |
| Eccentricity: | 0.0006588 |
| inclination: | 101.6502° |
| perigee height: | 138 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 153.3227° |
| argument of perigee: | 329.6103° |
| revolutions per day: | 16.48847764 |
| mean anomaly at epoch: | 30.4802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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