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 data is extracted from the following two-line orbital elements,
1 51044U 22002BN 24281.18236139 .00084205 00000-0 20985-2 0 9995
2 51044 97.3703 347.7731 0004250 6.7497 353.3805 15.39902165151602
| Epoch (UTC): | 07 October 2024 04:22:36 |
| Eccentricity: | 0.0004250 |
| inclination: | 97.3703° |
| perigee height: | 443 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 347.7731° |
| argument of perigee: | 6.7497° |
| revolutions per day: | 15.39902165 |
| mean anomaly at epoch: | 353.3805° |
| orbit number at epoch: | 15160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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